Kolb-Archive.digest.vol-fq

November 18, 2005 - December 14, 2005



      does not touch the hinges on the fuselage tube.  WE have seen some 
      installations where the hinges not only touch but actually are deflected with elevator
      
      movement.  THIS IS a very dangerous as the hinges could fatigue and crack with
      
      enough such bending.  There MUST be clearance on both sides as indicated. " 
      
      In my opinion the whole design of the tail attachment is ingenious. It allows 
      the tail to fold as well as allow for elevator movement in a very simple and 
      inspectable form.  You may not be able to see any movement at the rear of the 
      stabilizer  because the whole horizontal stabilizer and elevator floats on the
      
      control horn.
      
      Hope this helps,
      Steve Boetto
      
      
________________________________________________________________________________
Date: Nov 18, 2005
Subject: Re: My Mark III, not a crash
From: guyandjodi(at)bvillemn.net
> It is kept slightly loose so you can fold the > stabilizer up. This allows this to have some amount, ever so slight, of > vibration as you fly. This caused, over time, metal fatigue on the "L" > brackets. > --------------------------------- Roger, They sould not be slightly loose for folding they should be floating on that bolt. If you have the "L" brackets on the boom tube installed properly you would have had to add several washers to each side of the "L" brackets mounted to the horizontal stabilizer to tighten that bolt up. There should have been at least a 1/4in gap on both sides of the horizontal stab brackets so they could move (float) fore and aft as the elevator is moved up and down. Even if you can't see the movement fore and aft, it's there, and if you immobilize this connection by tightening up the bolt somethings gotta give. If you did have the gap in place for movement then please disregard this post. If you could please post pictures of the other horizontal stab mount. Just my .02 worth. Guy Swenson 3053B MKIII Xtra > > ________________________________________________________________________________
Date: Nov 18, 2005
From: Charles Blackwell <wozani(at)optonline.net>
Subject: MkII gear legs
My best guess, measuring on my MkII and also consulting the drawings=85. Is that the Firestar angle is definitely wrong for the MkII (I can send pics if you like). It makes the tops of the wheels lean inwards. I would go with something in the 30 degree angle range, which I measured on my plane. If you load it up heavy maybe you=92d want something like 35 degrees to allow the legs to flex a bit more and sit with the wheels still perpendicular to the ground. If in doubt, stick some 1 =BC=94 OD pipe in the sockets, or the old gear legs, and measure the angle from them to a level held perpendicular to the ground. Also, the MkII is very much like the MkIIIc in its design. I think the only real difference is the 6=94 tubing replacing the 5=94, and the flaps, all done to accommodate the higher horsepower engines. Charlie, MKII in NJ =93Ok, time for some more help. A good point was brought up about when I replace the gear legs and axle assemblies on my Mk II that the angle be correct for the wheels. The 1 1/4" gear legs are from the firestar and the standard axle assemblies from Kolb are welded at too much of an angle because the mk II sits low compared to the firestar. Travis at TNK said he would weld whatever angle I wanted. What do I want?=94 ________________________________________________________________________________
Date: Nov 18, 2005
From: Charles Blackwell <wozani(at)optonline.net>
Subject: MkII gear legs
My best guess, measuring on my MkII and also consulting the drawings=85. Is that the Firestar angle is definitely wrong for the MkII (I can send pics if you like). It makes the tops of the wheels lean inwards. I would go with something in the 28 degree angle range, which I measured on my plane. If you load it up heavy maybe you=92d want something like 25 degrees to allow the legs to flex a bit more and sit with the wheels still perpendicular to the ground. If in doubt, stick some 1 =BC=94 OD pipe in the sockets, or the old gear legs, and measure the angle from them to a level held perpendicular to the ground. Also, the MkII is very much like the MkIIIc in its design. I think the only real difference is the 6=94 tubing replacing the 5=94, and the flaps, all done to accommodate the higher horsepower engines. Charlie, MKII in NJ =93Ok, time for some more help. A good point was brought up about when I replace the gear legs and axle assemblies on my Mk II that the angle be correct for the wheels. The 1 1/4" gear legs are from the firestar and the standard axle assemblies from Kolb are welded at too much of an angle because the mk II sits low compared to the firestar. Travis at TNK said he would weld whatever angle I wanted. What do I want?=94 ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: MkII gear legs/MKII/MKIII Comparison
Date: Nov 18, 2005
| Also, the MkII is very much like the MkIIIc in its design. I think the only | real difference is the 6=94 tubing replacing the 5=94, and the flaps, all done | to accommodate the higher horsepower engines. | | | Charlie, MKII in NJ Charlie/All: Dennis Souder can speak to the above much better than I can. Please let me disagree with you a tad. The MKII is very much more like the original Twinstar, the first two place Homer Kolb kit. Basically, they enclosed a Twinstar to make a MKII. Structurally, the MKII is a Twinstar. Dennis S can correct me if I am wrong, please. About the only similarity between the two is the enclosed side by side cockpit, and the MKII is much smaller than the MKIII. The MKIII is a super strong "new" fuselage, six inch spars and tailboom, 10 rib wing sections, flaps, and does quite well with 582, 912 and 912S. I don't have any experience with the MKII. Never flown one. Dennis S and Dick Kuntzleman can certainly fill us in on that particular model. As far as gear leg/axle sockets, I prefer to set them up to have a good amount of positive camber. I think that makes the aircraft look better, fresher, than a Kolb sitting there in the grass or tarmac with a lot of negative camber, tired and worn looking. Does it handle any better on the ground. I don't know. On grass, doesn't matter. On pavement it might, but I have never flown a Kolb with a lot of negative camber on and off pavement. john h MKIII/912ULS Titus, Alabama ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: MkII gear legs/MKII/MKIII Comparison
Date: Nov 18, 2005
| The MKIII is a super strong "new" fuselage, six inch spars and | tailboom, 10 rib wing sections, flaps, and does quite well with 582, | 912 and 912S. Hi Gang: Forgot to add in my last post, the MKIII also sported a new "folding tail section" that took Dennis Souder and Homer Kolb a tremendous amount of time to come up with. No one else in the UL/Lt Plane world had anything like it. Using the MKIII tail section, to include the new folding mechanism, was the first Ferguson displayed at Sun and Fun 1991. Bill Ferguson's Fergie was awarded Sun and Fun Grand Champion Light Plane, 1991, or it may have been 1992. This alone was enough to irritate Homer Kolb and the rest of the Kolb gang, after putting so much effort into designing and developing. john h MKIII/912ULS Titus, Alabama ________________________________________________________________________________
From: Kirby Dennis Contr MDA/AL <Dennis.Kirby(at)kirtland.af.mil>
Subject: 912 in a Kolb.....in the UK...??
Date: Nov 18, 2005
Pat L, and KiwiMick - My Mark-III Classic, with a 912UL and BRS weighs 560 lbs. (254 kg). Does this fit your Microlight rules? Dennis Kirby N93DK, s/n 300 Cedar Crest, NM ________________________________________________________________________________
From: "Kolbdriver" <Kolbdriver(at)bellsouth.net>
Subject: Re:Forward Horizontal Stabilizer Attachment
Date: Nov 18, 2005
Steve, I am with you Steve. Sheet 3 of my Mark III plans specifically notes to leave room for the horizonal stab brackets to move fore and aft between the tail tube mounted "L" brackets. It even tells you that it will fatigue and break if it is not free to slide fore and aft on the AN3-10 bolt. When I made my first flight in the Mark III on Feb. 24, 2001 Bruce, Norm, and Danny came down to watch. Their inspection gave a thumbs up and after I took it a couple trips around the pattern Norm made a circuit or two in it. I think the temperature was in the 30s that day. While talking to them they pointed out the mistake that some builders make by restricting the movement at the forward horizonal stab. attachment. My hat is off to Roger for making a sucessful landing with such an inflight failure. Steven Green M3 400 hrs > Hi John, help me out here, I am not concerned here about whether or not the > L bracket is covered or not. Although I am a Kolb Neophyte, I think that I > understand the importance of having the joint free and moving. I am concerned if > people start boltin em up tight. or worse yet if the FAA mandates that it be > done based on the report of Roger's plane. The geometry of the elevator horn > moves in an arc and requires that the fore mounts can slide fore and aft. If > I am wrong here I will relinquish but I think I am on track. > > BTW, I'm ready for another Motocross Challenge, I've been practicing. > > Steve B > > ________________________________________________________________________________
Date: Nov 18, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Re: My Mark III, not a crash
Hi Steve, I checked my free play at this "L" bracket and had about 1/8" free play. I'm replacing all my "L" brackets and will leave a little more room for free play. I am also adding a second set of support cables to the leading edge of the horizontal stabilizer and this will prevent this from flapping up if I should ever have another type of failure. I hope never again. This should strengthen the tail area and still let it move. I also took the "L" brakets from under the fabric on the stabilizer so they can be inspected and replaced at 250 hrs. Thanks for the advise, Roger Lee In a message dated 11/17/2005 12:34:04 A.M. Eastern Standard Time, ssadiver1(at)yahoo.com writes: What broke was the stainless "L" bracket on the front inside edge of the horizontal stabilizer that allows the stabilizer to fold up. Looking at this I can see why it failed. It is kept slightly loose so you can fold the stabilizer up. This allows this to have some amount, ever so slight, of vibration as you fly. This caused, over time, metal fatigue on the "L" brackets. When I checked the other side I used a magnifying glass and found another crack. I would highly recommend that these stainless "L" brackets be changed at 250 hrs. and I would recommend putting in place a second horizontal stabilizer wire forward of the first. I learned this from J. Hauck, but did not put mine in place in time. My error. If I had put a second stabilizer wire in front of the first (top and bottom) it would have prevented the horizontal stabilizer from flying up. I am also going to add a second "L" bracket some where between 8"-10" behind the other. My Kolb will then be double wire braced and and have double "L" brackets. I never fold my plane up so I will also keep these bolts at the "L" bracket tight which will help with the minute vibration. To All, Question, I thought that since the trailing edge of the horizontal stab. moved up and down slightly with elevator changes that it was important to keep the forward joint at the L brackets loose. If you tightened it as suggested above would it not suffer from fatigue over time? Steve Boetto Firefly on Floats and Seabase Builder --------------------------------- ________________________________________________________________________________
Date: Nov 18, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Re: My Mark III, not a crash
Thanks for the advise. I am replacing my cables and adding a second set of wires like yours and using turnbuckles. Roger Lee Subject: Re: Kolb-List: My Mark III, not a crash At 10:29 PM 11/16/2005, you wrote: You can change those things to. You can even use swaged "machined" turnbuckles. I used them on the rudders and elevator wires too - gives you some adjustment when the wires stretch.. Not that there is anything wrong with the original equipment. It's just cleaner and not that expensive to do it like it should be done. http://www.mindspring.com/~possums/Modtail&swagedwires.jpg Just to put the rumors to rest. It was my Mark III Classic, 912s with 545 hrs TT. On take off and on downwind the passenger side horizontal stabilizer bracket broke and the stabilizer went straight up and stayed there. It was a little hard to control, but made a safe landing. Had to call NTSB because it was an in flight control failure. What broke was the stainless "L" bracket on the front inside edge of the horizontal stabilizer that allows the stabilizer to fold up. Looking at this I can see why it failed. It is kept slightly loose so you can fold the stabilizer up. This allows this to have some amount, ever so slight, of vibration as you fly. This caused, over time, metal fatigue on the "L" brackets. When I checked the other side I used a magnifying glass and found another crack. I would highly recommend that these stainless "L" brackets be changed at 250 hrs. and I would recommend putting in place a second horizontal stabilizer wire forward of the first. I learned this from J. Hauck, but did not put mine in place in time. My error. If I had put a second stabilizer wire in front of the first (top and bottom) it would have prevented the horizontal stabilizer from flying up. I am also going to add a second "L" bracket some where between 8"-10" behind the other. My Kolb will then be double wire braced and and have double "L" brackets. I never fold my plane up so I will also keep these bolts at the "L" bracket tight which will help with the minute vibration. I am also going to use turn buckles like J. Hauck instead of adjustable tangs to dial in my cable tightness. The NTSB may have suggestions to Kolb, I'm not sure what they will do? --------------------------------- ________________________________________________________________________________
Date: Nov 18, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Re: My Mark III, not a crash/Forward Horizontal Stabilizer
Attachment HI John, I removed the "L" brackets under the fabric and mounted them on the outside. I have also replaced all the "L" brackets and added a second set of cables with turnbuckles like your aircraft. I will also leave a little more free play in the "L" bracket mounts so the horizontal stabilizer can move a little more freely. Thanks for the tips. Roger Lee | The | crack can and usually does occur under the fabric at the first rivet. | | Steve Boetto Hi Steve B/All: Seems to me it is better to fix the bracket on the outside of the fabric for proper preflight inspection. May be prettier under the fabric, but not nearly as safe and functional. I always attach the horizontal stabilizer forward bracket after I cover and paint. However, all holes for bracket rivets are predrill and fitted prior to covering. john h MKIII/912ULS --------------------------------- ________________________________________________________________________________
Date: Nov 18, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Re:Forward Horizontal Stabilizer Attachment
Hi Steve, My "L" brackets had about an 1/8" free play. I have changed all my brackets and put them on the outside of the fabric on the horizontal stabilizer. I will also give them some more free play. I am also adding a second set of support cables on the front of the stabilizer and this will keep any failures from happening. It will be strong, but it will have the free play that it needs. Thanks for the help, Roger Lee Steve, I am with you Steve. Sheet 3 of my Mark III plans specifically notes to leave room for the horizonal stab brackets to move fore and aft between the tail tube mounted "L" brackets. It even tells you that it will fatigue and break if it is not free to slide fore and aft on the AN3-10 bolt. When I made my first flight in the Mark III on Feb. 24, 2001 Bruce, Norm, and Danny came down to watch. Their inspection gave a thumbs up and after I took it a couple trips around the pattern Norm made a circuit or two in it. I think the temperature was in the 30s that day. While talking to them they pointed out the mistake that some builders make by restricting the movement at the forward horizonal stab. attachment. My hat is off to Roger for making a sucessful landing with such an inflight failure. Steven Green M3 400 hrs > Hi John, help me out here, I am not concerned here about whether or not the > L bracket is covered or not. Although I am a Kolb Neophyte, I think that I > understand the importance of having the joint free and moving. I am concerned if > people start boltin em up tight. or worse yet if the FAA mandates that it be > done based on the report of Roger's plane. The geometry of the elevator horn > moves in an arc and requires that the fore mounts can slide fore and aft. If > I am wrong here I will relinquish but I think I am on track. > > BTW, I'm ready for another Motocross Challenge, I've been practicing. > > Steve B > > --------------------------------- ________________________________________________________________________________
From: "Ed Chmielewski" <edchmiel(at)mindspring.com>
Subject: Re: MkII gear legs/MKII/MKIII Comparison
Date: Nov 19, 2005
Hi John/all, Beyond the aesthetic aspect, positive camber is used in taildraggers (and to a lesser degree in tricycle gear) to aid in tracking during takeoff and landing. Part of the idea is that when landing on one wheel, the gear may deflect towards neutral and help keep the aircraft tracking straight. With negative camber, when the gear splays further out, it will tend to drag the aircraft away from the intended track. Of course, it just looks better, too. Ed in JXN (MI) MkII/503 ----- Original Message ----- From: "John Hauck" <jhauck(at)elmore.rr.com> Subject: Re: Kolb-List: MkII gear legs/MKII/MKIII Comparison > Charlie/All: > As far as gear leg/axle sockets, I prefer to set them up to have a > good amount of positive camber. I think that makes the aircraft look > better, fresher, than a Kolb sitting there in the grass or tarmac with > a lot of negative camber, tired and worn looking. Does it handle any > better on the ground. I don't know. On grass, doesn't matter. On > pavement it might, but I have never flown a Kolb with a lot of > negative camber on and off pavement. > > john h > MKIII/912ULS > Titus, Alabama > ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Nov 19, 2005
Subject: Re: slow day - laugh a bit
In a message dated 11/8/2005 11:48:06 A.M. Eastern Standard Time, ghaley(at)wt.net writes: Woody, I forwarded this to my wife and this is her response: "AND...the airplanes don't mind sleeping in the cold hanger with their pilots." Quoting woody : > > The list is kind of slow so I thought it would be a good time to add some > humour. This was recentley sent to me and I found it quite funny. > Unfortunately the girlfriend didn't. Guess its a pilot thing. > > > Airplanes usually kill you quickly; a woman takes her time. > >Airplanes can be turned on by a flick of a switch. > >Airplanes don't get mad if you do a "touch and go." and I merely say....."God Bless the feisty ladies" George Randolph firestar driver in The Villages, Fl ________________________________________________________________________________
From: "Silver Fern Microlights Ltd" <kiwimick(at)sfmicro.fsnet.co.uk>
Subject: Re: 912 in a Kolb.....in the UK...??
Date: Nov 19, 2005
Hi Dennis, Yep your bird would be legal in the UK at that weight, provided the VG's that I have got approved are fitted and we get the second weight increase we have applied for of 450kg. If the BRS was removed it would pass easily at our current weight. You obviously built a nice Kolb without getting carried away with too much paint etc. If Kolb's are built as per the book and care is taken with paint even us on this side of the pond can have a 912, look out mr Hauk I might be persuaded to go to the other side......... if I ever stop loving my Jab. ----- Original Message ----- From: "Kirby Dennis Contr MDA/AL" <Dennis.Kirby(at)kirtland.af.mil> Subject: Kolb-List: 912 in a Kolb.....in the UK...?? > > > Pat L, and KiwiMick - > > > My Mark-III Classic, with a 912UL and BRS weighs 560 lbs. (254 kg). > > Does this fit your Microlight rules? > > > Dennis Kirby > > N93DK, s/n 300 > > Cedar Crest, NM > > ________________________________________________________________________________
Date: Nov 19, 2005
Subject: Xtra
From: Todd Fredricks <flyingfox(at)copper.net>
Anyone know the panel dimensions and materials for the panel in an Xtra? I am trying to lay out a panel and need to know how much space I have to work with. Thanks, Todd -- Todd Fredricks, DO Flying Fox Services Visit my Blog at www.flyingfoxhangar.blogspot.com POWERED BY MAC ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Nov 20, 2005
Subject: Re: Rest of The Story
In a message dated 11/14/2005 8:23:59 P.M. Eastern Standard Time, biglar(at)gogittum.com writes: P.S. Jimmy, I really like your idea of the D.N.A. in the signature, but hafta agree with Larry. It'd become awkward in emails to others. Lar. xxxx Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com Larry, I can't believe you said that....awkward??!! ...NO WAY, It is BECAUSE of Jimmy that I now have this signoff signature which is always going to be part of my emails....thank you Jimmy.........well, does everyone get the drift that I most certainly did not say this with the proper respect to be shown Mr Biglar. He is most assuredly entitled to his position and I have mine. The other important observation is that I am soooooo far behind on my newsgroup emails. I visited the EAA chapter in Leesburg Fl yesterday and will probably join....nice group of guys there. Firestar driver from The Villages, Fl Rotax 447, 3 blade Ivo, KX, 1991 Do not Archive ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Nov 20, 2005
Subject: Re: Do N*t Archive Flag...
Come on guys, if you can build and fly an airplane, you can type three words to indicate that your message shouldn't be appended to the archive....by Matt Draille Geeez, how come we never looked at it that way? Firestar driver from The Villages, Fl Rotax 447, 3 blade Ivo, KX, 1991 Do not Archive ________________________________________________________________________________
From: "woody" <duesouth(at)govital.net>
Subject: Re: space cadets
Date: Nov 20, 2005
A story like that should be archived. ----- Original Message ----- > > > For those needing a reason of some kind for buying an Aircraft > > I have read many posts on the web site from members and on MMAIL who > are thinking about owning their own aircraft and looking for ways to > offset the cost of ownership. I have heard many reasons for and > against ownership. Why buy an aircraft? It's cheaper to rent and you > do not have all the hassle with maintenance, fuel and insurance. Well, > here is a little story that I think explains it all as to why I own my > own airplane. > > It was a beautiful Saturday morning. No winds and the temperature was > just right. So instead of mowing the lawn like my wife had planned for > me, I decided to go to the airport and take the Sport out for a run. > She yells back at me, "WELL IF YOU GO, TAKE YOUR SON WITH YOU." So I > ask my son. Want to go flying with dad? In which he says Yea, Can I > take my light saber? > > You see, my 9 year son thinks he is a Jedi Knight and that our Sport > is his personal X-Wing fighter. He is only 4'5 and has to sit on a > pillow in order to see over the glare shield and he always carries his > light saber just in case we land on a strange planet in which there > might be trouble or civil un-rest. Always prepared this one is. So > away we go. > > > THERE I WAS=85=85.. > > We were straight and level at around 6,000ft and I let him take the > controls of the X-Wing to do some turns to the left and right. Joshua > Approach called and said there was traffic at our 2'oclock 2 miles > opposite direction and My son said to me "Look over there dad, Tie > fighter coming right at us". I told him to steer clear of the Tie > Fighter because our lasers were out for repair and we were un-armed. > No reason to provoke a fight. > > So even though he is having a blast, I am starting to get a little > bored and thought, "Let's go do a practice approach on the ILS". So I > called Joshua Approach, requested the ILS 25 Approach to Palmdale Full > Approach and off we went. I maneuvered the X-Wing to the VOR and > started the turn outbound to the outer marker. Now my son is just > really enjoying this. At the outer marker, the blue light started to > flash and you could hear the BEEP in the headset. My Son jumps in and > said "That Tie Fighter has locked on to us" I said "That's Right" and > I started my evasive maneuver on the procedure turn. > > My Son is listening to the exchange between me and the controller and > wants to chime in on the conversion. I said to my son, "Just hang on; > I will give you a chance". I never should have said that because now > he is all excited to talk on the radio. As I start to turn inbound on > the turn, the Approach control said "Contact tower when established on > the localizer". So I told my young Padawan Learner "OK, when this > needle gets here on the dial, push the radio button and tell the tower > that 93 Romeo is inbound on the localizer". > > Now imagine this, I am giving basic instrument instruction to a 9 year > old, I cannot get adults to say this during training. So before I can > give him something simpler to say he keys the mike and says > > "REBEL BASE, THIS IS RED 5. WE ARE STARTING OUR ATTACK RUN ON THE > DEATH STAR". > > Good God. > > Now this post 9/11 and before I can key my mike and say anything, the > tower jumps on and says "RED 5, YOUR CLEARED FOR THE APPROACH TO THE > DEATH STAR. REPORTS HITS AWAY" > > Now I am waiting for the tower to add "And tell your dad to call this > number" But I hear nothing else. So we continue the approach. Now my > son is in heaven. This is real life stuff to him and he is doing > everything I tell him to do as far as tracking the needle. As we > approach the outer marker inbound, the light starts to flash and there > is that tone again. "Dad, the Death Star has a lock on us". Yes Son, > you keep on the approach, I will worry about the guns. > > Everything is going great and now we are approaching the middle > marker. My son has noticed the GPS has a red line with an airplane on > it and it ends at the Death Star. So he asks me "IS THAT A TARGETING > COMPUTER DAD?" Well of course it is, and it shows us where we are to > the target. So now he hears Obewan tell him to USE THE FORCE SCOTT and > he turns the GPS OFF. Tells me he is OK and does not need the > targeting computer because he is using the FORCE. > > Now the middle marker light flashes and the tone comes on. I apply > full power and the airplane,,,X-Wing,,, Starts a climb. I start the > turn to the missed approach path when my son keys the mike and says > "HITS AWAY". The tower answers back with "GOOD JOB RED 5, CONTACT > REBEL APPROACH ON 126.1" > > We go back to Mojave SPACEPORT, and I decide that the X-Wing needs a > bath. So out comes all the cleaning stuff and we spend the rest of the > day washing and waxing the turbo jets and laser pods. > > So you see. This is why I own my own aircraft. You cannot beat this > kind of quality time with your kids. And there is no way you can put a > price on that. > > > Jeff Bryant > Southwest Regional Director > Beech Aero Club > 1975 X-Wing Fighter Model B-19 > N6993R > > > > > > ________________________________________________________________________________
From: "pat ladd" <pj.ladd(at)btinternet.com>
Subject: Re: space cadets
Date: Nov 20, 2005
Hi Robert, What a great post. Have I your permission to forward it to a flying magazine?. With Christmas issues coming out soon I am sure they could use a good story like that. Incidentally is that the sort of post that should be archived or not. I would vote `Yes` MAY THE FORCE BE WITH YOU. Pat -- ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: Repairs underway - Highlights and LOWLIGHTS to be on Web
page
Date: Nov 20, 2005
That's really a shame, but, as you say, it could've been a lot worse. Hope to see you at MV this time. Lar. Do not Archive. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "John Bickham" <gearbender(at)bellsouth.net> Subject: Kolb-List: Repairs underway - Highlights and LOWLIGHTS to be on Web page > > Hello list, > > > Finally getting all my priorities right. Shop is cleared of all projects > that have taken up space to this point. Been working hard on my welding. > Really just getting started on the repairs to my Mark III Classic. For ________________________________________________________________________________
From: "Jim Ballenger" <ulpilot(at)cavtel.net>
Subject: MK III X 582 PERFORMANCE
Date: Nov 20, 2005
Larry T / Kolbers This weekend was great for flying Kolbs in southeast Virginia. Larry, I wanted to let you know what I got for a takeoff climb rate this morning. OAT was 54 degrees F, the plane with 20 gallons of fuel and me weighted 869 pounds at take off. The 582 was turning 6400 rpm and the ASI indicated 59/60 mph with the VSI initially showing 1000 fpm then 1100 fpm. After gaining a couple of hundred feet of altitude the VSI indicated 900 - 1000 fpm. Near the end of my climb at 1000 feet the VSI was indicating 700 - 800 fpm. I did a high speed run and could only get 87/88 mph IAS with the 9.5 degree pitch in the taper tip warp drive 3 bladed propeller. Jim Ballenger MK III X 582 Virginia Beach, VA ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: MK III X 582 PERFORMANCE
Date: Nov 20, 2005
| I did a high speed run and could only get 87/88 mph IAS with the 9.5 degree pitch in the taper tip warp drive 3 bladed propeller. | | Jim Ballenger | MK III X 582 | Virginia Beach, VA Jim B/Gang: Got a couple questions for you. What is the diameter of your Warp Drive? What was engine rpm at WOT, straight and level flight, 88 mph? What was gross weight of your Xtra during this test? Thanks, john h MKIII Titus, AL ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 20, 2005
Subject: Re: MK III X 582 PERFORMANCE
Jim/ Kolbers I performed the same drill this morning. My craft with me a 10 gal of fuel weighed 776 lbs. I pulled the nose up and held 58 - 60 mph and was showing 1000 fpm, then 1100 and down to 800-900 at 1000 ft. This was also with the taper tip and 6200 rpm. Later in the day (it was warmer) when taking off from another airport I could only get 5800 rpm. Got to do some checking there. Installed a trim tab on the elevator. Flew and adjusted same. Can now fly with two fingers for the most part. Have not done any high speed trials yet and usually cruise at 4500 to 5200 rpm which will give me 56 - 72 mph. Next the sand bags! Larry Tasker MKlllx 582 ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 20, 2005
Subject: Re: Xtra
The face of the pod (panel) measures 7" H x 11 1/4" wide. ________________________________________________________________________________
Date: Nov 20, 2005
Subject: Re: Xtra
From: Todd Fredricks <flyingfox(at)copper.net>
Cool. I appreciate the reply. Todd On 11/20/05 9:17 PM, "Cat36Fly(at)aol.com" wrote: > > The face of the pod (panel) measures 7" H x 11 1/4" wide. > > > > > > -- Todd Fredricks, DO Flying Fox Services Visit my Blog at www.flyingfoxhangar.blogspot.com POWERED BY MAC ________________________________________________________________________________
Date: Nov 20, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: FireFly Tail Cable Ends
FireFlyers & Kolbers, I have been watching the cable thimbles that pass through the tangs attached to the horizontal and vertical stabilizers. When I assembled the FireFly, I de burred the tang holes to remove the sharp corners and to provide a better load bearing surface to the thimble. At 194 hours one thimble above the horizontal stabilizer was showing enough wear that repair was required to prevent cable damage. I believe I need to increase tension in the cables to keep them from strumming. To repair the thimbles, I wrapped them with 0.016 inch thick brass to present a new wear surface to the tang. JB Weld was used to keep the wrap from sliding out of place on the thimble. If you would like to see how it was done, it can be seen at: http://www.thirdshift.com/jack/firefly/firefly120.html Hope to be back in the air tomorrow. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
From: Airgriff2(at)aol.com
Date: Nov 21, 2005
Subject: checking oil level on 912s
Hi Guys I have been flying a new 912s for a couple weeks now and each morning, before flight, I have gone through the procedure of hand turning the prop and listening for the gurgle sound of air in the oil tank to check the oil level. Up till now this was done on a cold engine. Yesterday after a flight,(engine warm), I wanted to check oil level and the second time I turned the prop the oil came out of the top of the tank, stayed there in the neck and gradually went down mabey a 1/2 " in 15 minutes but was still covering the handle on dip stick. Is this normal? Are you not supposed to check oil when the engine is warm? Fly safe Bob Griffin ________________________________________________________________________________
Date: Nov 21, 2005
From: Mark Anliker <manliker(at)uiuc.edu>
Subject: 912 break-in procedure???
Is there a Rotax 912 break-in procedure? I have the Installation, Maintenance, and Operator's Manuals, but don't see any recommended rpm and run-time guidelines like you see for 2-strokes. I am aware of the suggested oil system venting procedure prior to start up. Mark ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 912 break-in procedure???
Date: Nov 21, 2005
| Is there a Rotax 912 break-in procedure? | | Mark Hi Mark/Gang: Yes, there is a 912 breakin procedure. Same as every flight. Do not go full power until the engine oil temp has reached 120F. That's it. Actually, there is no breakin procedure. You may also start off using the oil you intend to operate with. 1994, I got my first 912. Has to run an organic oil for the first 25 hours. 2005, I got my 912ULS. Now we were authorized to start off with the oil we intended to run. In my case a full synthetic oil. However, when doing a lot of cross country flying requiring the use of a steady diet of 100LL, I use a semi-synthetic oil. In my case, Valvoline Durablend 5W40. When I am flying around home territory burning a steady diet of auto fuel, I use Shell Rotella 5W40 Full Synthetic. It is relatively cheap compared to others at 13.00 a gal in Wal*Mart. I also use Fram Tough Gard TG-3614 oil filters from Wal*Mart, and have for the last 11 or 12 years. See there. Ya got more than you bargained for. Guess I better qualify the above info. I am not telling anyone else to do the same thing I do with my engines. Simply telling you what I use. Take care, john h MKIII ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 21, 2005
Subject: Re: MK III X 582 PERFORMANCE
Rick; If you have a spare 912 laying around I'm sure Jim or I could use our MKlll as a flying testbed. I too am eager to see how that combo does. Larry Tasker MKlllx 582 ________________________________________________________________________________
From: blure2(at)comcast.net
Subject: SlingShot Purchase
Date: Nov 22, 2005
Hi, Group; I am contemplating the purchase of a use SlingShot. Two questions prevail: learning to fly it; and the quality of the aircraft. The answer to the first part may or may not nullify the second part. I am a low-time pilot, 75 hours, UL experience only. My plan is to pursue training in a tail-dragger aircraft. Instruction in Citabrias is available locally. It is my intent to train to a point of proficiency in a tail-dragger of as close to similar performance as possible. My concern is that, after a conversation today with Travis at Kolb, the SlingShot is a difficult plane to fly and I am placing myself and the plane in a risky position. Should adequate training be sufficient to raise my competence to an acceptable level, then I will need to address question number two. I have found a SlingShot for sale in Summitville, TN. With regard to question number one, the owner, suffering from impatience, attempted to fly the plane, without benefit of proper training, and managed to flip it on to it's back. I have been told that the damage consists of a broken nosecone, and wrinkled wing. The owner purchased and built a new wing, which needs to be mounted and squared up to the fuselage, covered and painted. A new nosecone needs to be purchased and installed as well. If I determine, with your help, that I will move forward with the SlingShot, I would like to have the plane inspected on my behalf. Can someone provide me with the names and contact information of qualified individuals in the Nashville/Chattanooga areas that can perform a detailed inspection of the plane? Thank you, Bob Blu Centennial, CO Hi, Group; I am contemplating the purchase of a use SlingShot. Two questions prevail: learning to fly it; and the quality of the aircraft. The answer to the first part may or may not nullify the second part. I am a low-time pilot, 75 hours, UL experience only. My plan is to pursue training in a tail-dragger aircraft. Instruction in Citabrias is available locally.It is myintentto train to a point of proficiency in a tail-dragger of as close to similar performance as possible. My concern is that, after a conversation today with Travis at Kolb, the SlingShot is a difficult plane to fly and I am placing myself and the plane in a risky position. Should adequate training be sufficient to raise my competence to an acceptable level, then I will need to address question number two. I have found a SlingShot for sale in Summitville, TN. With regard to question number one, the owner, suffering from impatience, attempted to fly the plane, without benefit of proper training, and managed to flip it on to it's back. I have been told that the damage consists of a broken nosecone, and wrinkled wing. The owner purchased and built a new wing, which needs to be mounted and squared up to the fuselage, covered and painted. A new nosecone needs to be purchased and installed as well. If I determine, with your help, that I will move forward with the SlingShot, I would like to have the plane inspected on my behalf. Can someone provide me with the names and contact information of qualified individuals in the Nashville/Chattanooga areas that can perform a detailed inspection of the plane? Thank you, Bob Blu Centennial, CO ________________________________________________________________________________
From: "woody" <duesouth(at)govital.net>
Subject: Re: Any tricks for taking straightening bent tubes?
Date: Nov 21, 2005
Try putting your cars scissor jack between the tubes. Put wood betwen top and bottom so you don't scratch the tubes. A small hydrolic jack will work great if it will fit in. Heating red hot may help the bending also. I don't know what you are bending so this is all guessing. You may need to block other tubes so that you don't bend the wrong tube. Using a long 2x4 on the base will also distribute the pressure along the tube. ________________________________________________________________________________
From: "woody" <duesouth(at)govital.net>
Subject: Re: Rest of The Story
Date: Nov 21, 2005
I was raised not to pick on the defenseless. Lucky he is out in the middle of the deseret where no one can check for sure on the tooth ache > > Speedy Lar? Speedy Lar? Did I read that right? > ok, who's going to step up to the plate on that one? ;) > > > > > ________________________________________________________________________________
From: "duncan mcbride" <duncanmcbride(at)comcast.net>
Subject: Re: Repairs underway - Highlights and LOWLIGHTS to be on Web
page
Date: Nov 22, 2005
Hey John, good to hear from you. I've been working on 319DM for about a year now, I hope it goes more quickly for you. I hope to get some pictures up on the web too. I just finished spraying silver on the wings, and I have to say, it was the great job you did on your aileron and flap gap seals that inspired me to abandon the bookbinding tape and do it according to the plans. Now all I have to do is flip the wing-flap-aileron assembly over to spray the color and I'll be ready to attach the hinges. Luckily I have more help than when I built the first set. I saw the damage to your nose cone and I'd say that is repairable. It depends on how much you've had to customize it to fit your plane. I had the nose ripped off mine, but I had done enough fiberglas work to make a battery tray and strengthen it that it was easier to fix than start over. Good thing I was able to find the sliced off part - the hurricane blew it back into a corner of the hanger where it just rattled around, it could have blown it to Georgia... See you at the homecoming, Duncan ----- Original Message ----- From: "John Bickham" <gearbender(at)bellsouth.net> Subject: Kolb-List: Repairs underway - Highlights and LOWLIGHTS to be on Web page > > Hello list, > > > Finally getting all my priorities right. Shop is cleared of all projects > that have taken up space to this point. Been working hard on my welding. ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: 503 de-carbon
Date: Nov 23, 2005
Group, Recently, I pulled the exhaust from my 503 to check for carbon. I had 100 hours since my last de-carbon. I have never been able to get a good feeling from checking through the exhaust port, and this time was no exception, so I took the engine off and pulled the heads and cylinders. I found one oil ring stuck on an end and the other oil ring had a 3/8" piece broke off the end. I have no idea what caused the ring to break or how long it had been that way, but I was glad that I decided to do a complete check. As far as the stuck ring goes, is this normal after only 100 hours? After my last de-carbon, I switched to oil injection and Pennsoil air cooled. Also, I try to keep the rpm's and temps up to avoid carbon. All I can think of is that maybe I didn't remove enough carbon from the ring lands last time. I used to use Amsoil and the carbon from that oil is really hard. I always feel better about flying after I have seen the pistons and cylinders. Carbon may be a concern for me but wear isn't. The rings and cylinders measured well within new specs after 200 hours. John Jung Firestar II N6163J Surprise, AZ ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: test
Date: Nov 24, 2005
please ignore... LS N646F ________________________________________________________________________________
From: DAquaNut(at)aol.com
Date: Nov 23, 2005
Subject: Re: Cleaning Stits Polytone
List, I checked the archives and found nothing. What works best to clean Polytone ? Is there any thing I should stear clear of that might damage the finnish? Ed ( In Houston) ________________________________________________________________________________
From: DAquaNut(at)aol.com
Date: Nov 23, 2005
Subject: Re: Firefly rigging and trim
Group, I have been doing fast taxis in my Firefly. I have had my left wing to lift off twice at about 40 mph. Is this normal for a Kolb that is adjusted properly? Is this a result of the prop blast on the tail surface? Ed (In Houston) ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 25, 2005
Subject: Engine Noise and Radio's
A general question to all kolbers: Has anyone found a good headset and mic that works with these noisy engines we use? I can talk and hear with my Dave Clarks at middle Rpm's but above 5000 it is almost senseless to try and communicate. There are several options on the market but its like picking a Medicare prescription plan. Thanks Larry Tasker MKlll x 582 ________________________________________________________________________________
Date: Nov 25, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Re: Engine Noise and Radio's
My buddy in the hangar next door added an ANR kit to his David Clark's. Last week I took the FSII for a flight and was amazed at how much quieter it was. Very impressive. Later, I was on the ground listening when he went to the Big airport, talking to ATC, he sounded good and he could hear ok, and they had no trouble hearing him. Richard Pike MKIII N420P (420ldPoops) > >A general question to all kolbers: > >Has anyone found a good headset and mic that works with these noisy engines >we use? I can talk and hear with my Dave Clarks at middle Rpm's but above >5000 it is almost senseless to try and communicate. There are several >options on >the market but its like picking a Medicare prescription plan. > >Thanks >Larry Tasker >MKlll x 582 > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: ANR
Date: Nov 25, 2005
| I have a noise canceling unit made by PILOT. I have this set for 6 years in helicopters and planes. I really like my headset. The model is the PA 17-79T DNC XL. The price is about $450. Also check this link: | www.planeandpilotmag.com/content/buyersguide/headset2000.html | | Roger Lee Hi Roger L/Lanny F/Gang: I checked out the referenced web page but did not see the headset I bought last May, the DRE Communications 6000enr Headset http://www.avionicswest.com/articles/DRE6000enr.html#6000 I have done one flight out West, up and down the West Coast, and back to Alabama with it. Costs $279.00 and worth every penny. In addition, this set comes with a small control box that uses 2 ea 9V bats, although it operates on only one quite well. However, it will operate more than twice as long on two batteries. Another great feature is the power adapter to allow the set to operate directly off the aircraft 12VDC system. I never use the 9V bats although they are installed. Highly recommend the DRE 6000. john h MKIII Titus, AL ________________________________________________________________________________
Date: Nov 25, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Good midnight reading on 4 stroke oil
HI John, Found some very good articles on oil if you care to read them. Some of the other Kolb'ers might also find them interesting as well. Just click on the links. www.xs11.com/stories/croil96.htm www.nordigroup.us/oil.htm#oil%20change%20intervals No serious point here, but some good information and something to help with facts and myths about oils. Roger Lee --------------------------------- ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Test plse ignore
Date: Nov 26, 2005
test LS ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: ANR
Date: Nov 26, 2005
Lanny and Group, When I used a Comtronics set, the mic would pick up the sound of the engine and put it through the speakers, making it all but impossible to communicate. I switched to a DRE intercom and that problem went away. It is important to have a unit with a good squelch. John Jung Firestar II N6163J Surprise, AZ On Nov 26, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > Happy Thanksgiving to all, Where do you buy an ANR kit, and do you > think it will work with a Comtronics dual-com? My set up works well, however, there is always the drone of the engine coming through the earphones. ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Engine Noise and Radio's
Date: Nov 26, 2005
Larry and Group, I use the DRE 6000 and I am really happy with it. But here something really inexpensive that can make a significant improvement with any headset: Foam ear plugs. They really add to the noise reduction and the headset volume can be turned up so that hearing voices is no problem. I like the Remington brand best. They are soft and comfortable. Some others are very dense and actually work too well. John Jung Firestar II N6163J Surprise, AZ On Nov 26, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > Has anyone found a good headset and mic that works with these noisy > engines > we use? ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Prop noise
Date: Nov 26, 2005
Group, Recently someone suggested that some of the prop noise for large diameter props was coming from the prop tips as they passed close to the boom tube. Whoever suggested that was "right on". For the last year or two, I had my engine raised up about an inch. It was raised so that I could fold the wings with a two blade IVO in the horizontal position. When I put the engine back on after my recent de-carbon, I put it back in the normal position. On the first flight, I noticed a significant increase in prop noise. The gap between the prop tip and the boom tube is now about an inch. Before it was close to two inches. So, now I have to decide if I should put the engine back up, or cut the 68" prop down to 66", or both. Ideas? John Jung Firestar II N6163J Surprise, AZ ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 26, 2005
Subject: Re: Engine Noise and Radio's
Thanks to all who have (and will) responded . Good input on a common problem most of us share. I am as concerned with the TX as well as the RX ability of a unit because of the backround noise (as some have mentioned). Last week while talking to Dover Approach (Checking X-ponder operation) The controller had to ask me to repeat three times and give me a code twice. We finally connected when I pulled the throttle back. Not what I want for normal operation. Larry Tasker MKlllx 582 ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Engine Noise and Radio's
Date: Nov 26, 2005
| The controller had to ask me to | repeat three times and give me a code twice. . | | Larry Tasker Larry T/Gang: A large capacitor, about 22,000 mf, will do wonders for reducing rf noise on the tx and rx sides of your radio. Install it on the 12DCV side of the regulator/rectifier, close to the reg/rec, insuring you have a good ground. The capacitor will have a + and - connector. It will soak up a lot of extraneous noise. Also, the headset you use has a lot to do with radio performance. I complained for a year that my buddies radios were poorly transmitting. Had a hard time hearing and understanding them. I had used David Clark head sets, H-10-40, for years, but it was the DC sets that were going belly up, not receiving or transmitting well. Was also getting a squeal when transmitting. Blamed it on the little ICOM A3 radio. Bought a new radio and had the same problem. May 2005, bought the DRE6000 ENR headset and my radio and my buddies' radios problems went away. It was all headset. Take care, john h ________________________________________________________________________________
Date: Nov 26, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Re: Engine Noise and Radio's
I have found reducing power to be the most consistently successful way of talking to ATC. You don't need a huge reduction, 4,800 rpm will usually do it. Something no one else has mentioned as a factor in engine noise is that there is normally no sound insulation between the engine and the cockpit. Several people have commented that flying in my MKIII is quieter than the usual Kolb, and we finally figured out that it is because the main gas tank is located in the gap seal. Having a dense, thick-walled fiberglass gas tank between me and the engine is a big factor in reducing engine noise. That, plus the MKIII has a contiguous fabric insert that spans the full upper fuselage between the wings. For those flying MKIII's, how about installing a lightweight foam sound-absorbing insert atop the fabric spanning the gap seal? And blocking off any holes or openings within the gap seal that open into the cockpit area? Richard Pike MKIII N420P (420ldPoops) > >Thanks to all who have (and will) responded > >. Good input on a common problem most of us share. > >I am as concerned with the TX as well as the RX ability of a unit because of >the backround noise (as some have mentioned). Last week while talking to >Dover Approach (Checking X-ponder operation) The controller had to ask me to >repeat three times and give me a code twice. We finally connected when I >pulled >the throttle back. Not what I want for normal operation. > >Larry Tasker >MKlllx 582 > > ________________________________________________________________________________
Date: Nov 26, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Re: Engine Noise and Radio's
Hi Richard, I hate to say it, but sometimes we have to invest more money in some things than we want to. In this case a good ANR headset is worth the money. Usually, but not always, a $250 set is not as good as a $450-$500 set. My Pilot series PA17-79 DN XL works very well in all the noise. It cost approximately $450. I bought it for use in my Helicopter because it is good for higher ambient noise areas. Several of the helicopter headsets have better ratings because of noise. (not all) I have no problem hearing or transmitting in my Mark III. I am hard of hearing and I like the fact also that I can turn the radio to everyone elses comfort and turn the volume up for me. I would highly recommend this headset. Thanks for all the help on this site, Roger Lee Richard Pike wrote: I have found reducing power to be the most consistently successful way of talking to ATC. You don't need a huge reduction, 4,800 rpm will usually do it. Something no one else has mentioned as a factor in engine noise is that there is normally no sound insulation between the engine and the cockpit. Several people have commented that flying in my MKIII is quieter than the usual Kolb, and we finally figured out that it is because the main gas tank is located in the gap seal. Having a dense, thick-walled fiberglass gas tank between me and the engine is a big factor in reducing engine noise. That, plus the MKIII has a contiguous fabric insert that spans the full upper fuselage between the wings. For those flying MKIII's, how about installing a lightweight foam sound-absorbing insert atop the fabric spanning the gap seal? And blocking off any holes or openings within the gap seal that open into the cockpit area? Richard Pike MKIII N420P (420ldPoops) > >Thanks to all who have (and will) responded > >. Good input on a common problem most of us share. > >I am as concerned with the TX as well as the RX ability of a unit because of >the backround noise (as some have mentioned). Last week while talking to >Dover Approach (Checking X-ponder operation) The controller had to ask me to >repeat three times and give me a code twice. We finally connected when I >pulled >the throttle back. Not what I want for normal operation. > >Larry Tasker >MKlllx 582 > > --------------------------------- ________________________________________________________________________________
Date: Nov 26, 2005
From: jerb <ulflyer(at)verizon.net>
Subject: Re: Firefly rigging and trim
Ed, and all, If your going to do any taxiing at all, make sure you seat belt is fastened and the plane is ready to fly (preflight and adequate fuel on board for a hour or so) just in case it gets air bourne. Heard and see the results of to many panic situations where the plane get off the ground. The pilot panics because he's not ready to fly and splats it back down on the runway and busts the airplane. Be ready to fly and if it gets in the air fly the airplane - circle until you settle down and then set up for a nice easy approach to touch down. jerb At 09:05 PM 11/23/2005, you wrote: > > >Group, > > I have been doing fast taxis in my Firefly. I have had my left wing to >lift off twice at about 40 mph. Is this normal for a Kolb that is adjusted >properly? Is this a result of the prop blast on the tail surface? > > Ed (In Houston) > > ________________________________________________________________________________
Date: Nov 26, 2005
From: jerb <ulflyer(at)verizon.net>
Subject: Re: Prop noise
When I was at Oshkosh back in 95 looking at the FireFly, Dennis commented about the noise being generated by the prop passing the trailing edge of the wing, they added a spacer to increase the clearance and found it reduced the noise also. John Hack might know more about this. jerb At 06:15 AM 11/26/2005, you wrote: > >Group, > >Recently someone suggested that some of the prop noise for large >diameter props was coming from the prop tips as they passed close to >the boom tube. Whoever suggested that was "right on". For the last year >or two, I had my engine raised up about an inch. It was raised so that >I could fold the wings with a two blade IVO in the horizontal position. >When I put the engine back on after my recent de-carbon, I put it back >in the normal position. On the first flight, I noticed a significant >increase in prop noise. The gap between the prop tip and the boom tube >is now about an inch. Before it was close to two inches. So, now I have >to decide if I should put the engine back up, or cut the 68" prop down >to 66", or both. Ideas? > >John Jung >Firestar II N6163J >Surprise, AZ > > ________________________________________________________________________________
From: "pat ladd" <pj.ladd(at)btinternet.com>
Subject: Re: DNA
Date: Nov 26, 2005
never thought that the extra tidbits being archived as being a problem other than taking some extra disk space on Matt's disk bank. >> Hi Jerb, I agree. Search engines are pretty good provided that they have a handle to latch on to and a few extra items should not cause a real problem. The problem of not updating the subject line is I am afraid not confined to this list. The topic is a running grouse on almost all I would suspect. Things seem to have settled down now. Cheers Pat -- ________________________________________________________________________________
From: DAquaNut(at)aol.com
Date: Nov 26, 2005
Subject: Re: Prop noise
In a message dated 11/26/2005 6:15:32 A.M. Central Standard Time, jrjungjr(at)yahoo.com writes: I had my engine raised up about an inch. It was raised so that I could fold the wings with a two blade IVO in the horizontal position. When I put the engine back on after my recent de-carbon, I put it back in the normal position. On the first flight, I noticed a significant increase in prop noise. The gap between the prop tip and the boom tube is now about an inch. Before it was close to two inches. So, now I have to decide if I should put the engine back up, or cut the 68" prop down to 66", or both. Ideas? John, I dont have any advice, But I would like to know how you raised your engine that 1" and how noticeable of an effect it had on flight characteristics. Ed ( In Houston) ________________________________________________________________________________
From: DAquaNut(at)aol.com
Date: Nov 26, 2005
Subject: Re: Firefly rigging and trim
In a message dated 11/26/2005 12:30:12 P.M. Central Standard Time, ulflyer(at)verizon.net writes: Some thing you might want to consider is changing out the 400x6 Shin tires to 600x6. Guy Morgan who bought our FF made a post in the past about changing out the tires and it improving high the speed handling characteristics claiming it settled it down. Reference the message below: Jerb, I found out along time ago, Just like Ole Bro Beauford told me, He got rid off those little wheels and tires right off.. I have the 6" wheels which make a BIG difference. I was just wondering if a properly rigged Kolb had a tendency to lift the left wing first, as viewed from the pilots seat. Ed (In Houston) ________________________________________________________________________________
From: "George T. Alexander, Jr." <gtalexander(at)att.net>
Subject: Engine Noise and Radio's
Date: Nov 26, 2005
Kolbers: Based on a number of threads over the last several months, I decided to go for the DRE6000 ENR. Just prior to acquiring the new headset, I also had gotten a new Icom A23. (Santa came early this year.) Early in my use of the combination, I noticed once when, I was testing the setup on the ground, not in the plane, I developed a very loud squeal when keying the transmitter. Didn't think much about it at the time. Later, when doing some Googling re: the A23 and available accessories, I ran across an evaluation of the A23 by someone from Avionics West (which is where John Hauck got his DRE6000 I think) that this squeal was common between the A23 and a number of good headsets. Writer says the two will not work together. (Evaluation write-up at: http://www.avionicswest.com/articles/a23.htm ) The evaluator eludes to the problem being more in the relationship of the headset and the headset adapter. I would tend to agree since rigged in my FSII, (the one that Mike Shackleford thinks is retired)..... radio strapped to my leg, cables under my leg and up my side to the headset and ENR box in my shirt pocket... no squeal using the combination. Same condition whether using the rubber ducky or the $5 coax antenna. My $.02 worth. George Alexander http://gtalexander.home.att.net -----Original Message----- From: owner-kolb-list-server(at)matronics.com [mailto:owner-kolb-list-server(at)matronics.com]On Behalf Of John Hauck Subject: Re: Kolb-List: Engine Noise and Radio's <<>> Larry T/Gang: A large capacitor, about 22,000 mf, will do wonders for reducing rf noise on the tx and rx sides of your radio. Install it on the 12DCV side of the regulator/rectifier, close to the reg/rec, insuring you have a good ground. The capacitor will have a + and - connector. It will soak up a lot of extraneous noise. Also, the headset you use has a lot to do with radio performance. I complained for a year that my buddies radios were poorly transmitting. Had a hard time hearing and understanding them. I had used David Clark head sets, H-10-40, for years, but it was the DC sets that were going belly up, not receiving or transmitting well. Was also getting a squeal when transmitting. Blamed it on the little ICOM A3 radio. Bought a new radio and had the same problem. May 2005, bought the DRE6000 ENR headset and my radio and my buddies' radios problems went away. It was all headset. Take care, john h ________________________________________________________________________________
Date: Nov 26, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Engine Noise and Radio's
Kolbers, If you get a squeal in the headset when you press the push to talk button, more than likely it is a rf (radio frequency) feed back problem. I had this problem and solved it with a snap on ferrite bead. They are inexpensive. I have purchased them from: http://www.allelectronics.com/cgi-bin/category.cgi?category=235&type=store If your microphone adapter lead is too short, you may not have enough length to wrap it through one turn. But if you can, it is a much less expensive fix than purchasing a new head set. These snap on ferrite beads are used on the computer accessory leads. If you have a junk box, you may have one you can try. You can see the one I put on my radio at the top of: http://www.thirdshift.com/jack/firefly/firefly110.html I used to have ignition noise, but I eliminated it by moving the mag kill switch from under the seat to close to the engine. I activate the normally open switch with woven fish line. It is lighter than wire and cannot radiate ignition noise. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
Date: Nov 26, 2005
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Prop noise
John Jung wrote: > >Group, > >Recently someone suggested that some of the prop noise for large >diameter props was coming from the prop tips as they passed close to >the boom tube. Whoever suggested that was "right on". For the last year >or two, I had my engine raised up about an inch. It was raised so that >I could fold the wings with a two blade IVO in the horizontal position. >When I put the engine back on after my recent de-carbon, I put it back >in the normal position. On the first flight, I noticed a significant >increase in prop noise. The gap between the prop tip and the boom tube >is now about an inch. Before it was close to two inches. So, now I have >to decide if I should put the engine back up, or cut the 68" prop down >to 66", or both. Ideas? > >John Jung >Firestar II N6163J >Surprise, AZ > Until you get up near 200 mph, the larger the prop diameter, the better its efficiency in converting torque to thrust (the techies talk about 'mass flow' through the prop). Surprisingly small changes in diameter can make significant differences in low speed thrust. Did it fly ok with the elevated thrust line? Charlie ________________________________________________________________________________
Date: Nov 26, 2005
From: Mike Pierzina <planecrazzzy(at)yahoo.com>
Subject: Mounting ELT
http://www.wingsforum.com/viewtopic.php?p=3377#3377 --------------------------------- ________________________________________________________________________________
From: "John Cooley" <johnc(at)datasync.com>
Subject: Warp Drive prop question
Date: Nov 27, 2005
Hi Guys, Got a question for you Warp Drive folks or anyone that can enlighten me. I bought a 66" 2 blade taper tip prop for my MK II that I have been sprucing up to sale. I didn't like the GSC prop that was on it is the reason for switching. Anyhow back to the question. With the GSC and the Powerfin prop on my FS II I would always set the prop for about 6200~6300 static rpm's to achieve the 6600~6700 level flight WOT rpm's. The prop unloads in flight and turns higher rpm's, right? Well, with this prop I first set it up turning 6200 rpm's on the ground and took it up for a test flight. Max level flight rpm's was about 5700~5800 rpm's and the engine was real slow to rev up. This scared me for a minute or two as I thought something was going wrong with the engine. I then went back and adjusted the prop twice more and wound up with 6600 static and 6400 WOT level flight. This prop came off a Firestar and supposedly vibrated real bad and this was the reason for selling. I fixed the vibration problem, but am puzzled by the lower rpm's in WOT level flight. The climb rate seems about normal but I really couldn't tell as it was very bumpy yesterday. My butt came out of the seat a few times while descending for landings. I have heard of constant speed blades on Warp drive props. Is this possibly the reason for the lower flight rpm's I am seeing? Thanks, John Cooley -- ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Warp Drive prop question
Date: Nov 27, 2005
| I have heard of constant speed blades on Warp drive props. Is this possibly | the reason for the lower flight rpm's I am seeing? | | Thanks, | John Cooley John C/Gang: Yep. Set pitch so it will bump the red line at WOT straight and level flight. You will then obtain the best cruise and climb. That's the way it works, and that is the way the two strokes, especially, like to be set up. 5,800 rpm is about 75% power. I ran my two strokes, primarily, at this rpm and had very good luck with them. I run the 912/912S at 75% power and higher. My 3 blade taper tip Warp Drive is pitched for 5,400 rpm static. A few feet into take off roll, the rpm drops 100 to 150 rpm and stays that way throughout WOT climbs. WOT, straight and level is 5,500. john h MKIII/912ULS ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop noise
Date: Nov 27, 2005
Ed and Group, I raised the engine by using longer bolts and washers and nuts for spacers. I measured it since my last post and it was closer to 1/2 inch that I had raised it. But the sound difference was noticeable. The bolts are long enough to go up 3/4 inch, so I will try that. John Jung Firestar II N6163J Surprise, AZ On Nov 27, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > John, > > I dont have any advice, But I would like to know how you raised > your > engine that 1" and how noticeable of an effect it had on flight > characteristics. > > Ed ( In Houston) ________________________________________________________________________________
From: "J.D. Stewart" <jstewart(at)inebraska.com>
Subject: Warp Drive prop question
Date: Nov 27, 2005
It's amazing how the same subject comes up about the same time on different lists. I've seen this time and time again. Here's an exchange from the Titan list (pretty long, but worth the read) during the last few days concerning this very thing: -----Original Message----- From: Titanaircraft(at)yahoogroups.com [mailto:Titanaircraft(at)yahoogroups.com]On Behalf Of Kimberly Panos Subject: Re: [Titanaircraft] tapered prop Thom, By eliminating prop area (wing area), it reduces the amount of total thrust (lift if a wing) the prop is capable of at a given RPM (speed). As a conventional piston engine's RPM increases, horsepower increases in a relatively linear fashion (to a point), but the load imposed on the engine by the prop increases by the square. This means that when the prop load matches the available horsepower, the engine RPM can't increase (kind of like hitting a wall). The tip is where the most lift and drag can be created. After a conventional piston engine reaches it's peak design torque RPM(determined by bore/stroke combination, cam, compression, heads, induction system, manifolds, etc.), the torque begins to fall while the prop load increases. How and where you reduce the area is crutial. For example, if you had an unlimited controllable power source that you could turn both props to 3000 RPM, the straight blade, non-tapered tip would produce more thrust and require more power, even though the tip speed is the same. It kind'a boils down to physics. You don't get anything for free. By tapering the tips, the taper tip prop isn't capable of producing the same thrust at the same RPM as before, but allows the engine to get to its peak operating range which would allow the maximum thrust that the engine/prop combo is capable of while maintaining the prop speed (tip speed). It's much more efficient than running a short, stubby prop or stubby props with many blades. That's another reason two blades provide better performance than three for the same application. It allows a larger diameter and more pitch for the same load. If they weren't any more noisy on a pusher, you can bet we'd be running two-blade props instead of three-blade (as long as they clear the tailboom). I'm sorry can't think of a real simple explanation for that one. I think I'd better quit here since the more I elaborate, the more complicated it's getting. cheers, --Kimberly ----- Original Message ----- From: "Thom Riddle" <jtriddle(at)adelphia.net> Subject: [Titanaircraft] tapered prop > Kimberly, > > Thanks for the explanation and it sounds plausible but confusing a bit, at > least to me, for > two reasons. > 1) How does the Warp Drive prop NOT change rpm much from relatively low > speed Vy > climb under full throttle, to straight and level full throttle speeds at > least 30-40 mph > faster, without a flexing or pitch change? > 2) My Woodcomp prop is gradually tapered along the chord from about 25-30% > radius out > to about 95%, then sharply tapered the last 5% or so. If it the tapering > that enables this > strange phenomenon and not flexing lateraly (effectively changing pitch > dynamically), then > my Woodcomp should show similar rpm behavior, wouldn't it? > > I'm not questioning you explanation just trying to understand why the Warp > does what it > does and others that look similar do not. The leads me to believe that > their is some > dynamic lateral flexing (pitch changing) in the Warp that is not happening > in the > Woodcomp and others. It does not take much pitch change to make a big > difference in > rpm. > > Thom > --- In Titanaircraft(at)yahoogroups.com, "Kimberly Panos" > wrote: >> >> Thom, >> >> The so-called CS effect of a warp really isn't because the blades warp. >> I >> haven't seen the tips warp or flex on ours at all, even on near full >> throttle runups. What it does is provide less load at the tip (where the >> load is hardest to turn) to allow the engine to get up to it's peak >> horsepower, but keep the prop tip speed alive while doing so. This keeps >> the efficiency up and the load down. Just like a glider wing compared to >> the wing on the Tornado. While the two could have the same square >> footage, >> the glider wing (due mainly to its high aspect ratio wing), it is much >> more >> efficient (more lift, less drag), but not as stout enough to carry heavy >> loads. Notice that the majority of all certified modern aircraft (except >> a >> few like the Archer, trainers, etc) use a tapered chord wing, as does the >> propeller on mainly piston prop planes because they are more efficient >> and >> not because they twist or warp. A constant chord wing is just cheaper >> and >> easier to produce, provides docile characteristics, and keeps speeds down >> for some aircraft categories. The main reason why you'll see those >> mostly >> on metal-winged kit planes and trainers. >> >> The nice thing about being able to taper a finished prop is to customize >> the >> prop load while keeping efficiency up, unlike most other composite props >> where you can only chop them off for length -- a dismal experience we had >> with Ivo where the medium HP blades were just down-right too wide for the >> high RPM requirement of the Jabiru. >> >> --Kimberly And one of the first posts on the subject: From: "Barry Weinzirl" <rans9(at)wwt.net> Date: Thu Nov 17, 2005 9:11 am Subject: Re: [Titanaircraft] Re: Propwash, Texas to Santa Ynez, CA: The Very Long Story If you run a warp drive taper tip you will usually static more rpm then what you turn as you get rolling. I have the same thing on my 503. I will static a 100rpm or more than what I turn in the climb. It has to do with parts of the prop being stalled until you get some forward air moving through it. At least that is what warp says. And they only gain a few hudred between climb and strainght and level. They are very tight. Barry There you go. Hope that helps. Warp Drive Dealer, J.D. Stewart UltraFun AirSports, LLC www.ultrafunairsports.com Titan Aircraft E-mail list http://groups.yahoo.com/group/Titanaircraft/ Challenger E-mail list http://groups.yahoo.com/group/FlyChallenger/ > > Hi Guys, > Got a question for you Warp Drive folks or anyone that can enlighten me. I > bought a 66" 2 blade taper tip prop for my MK II that I have been sprucing > up to sale. I didn't like the GSC prop that was on it is the reason for > switching. Anyhow back to the question. With the GSC and the Powerfin prop > on my FS II I would always set the prop for about 6200~6300 > static rpm's to > achieve the 6600~6700 level flight WOT rpm's. The prop unloads in > flight and > turns higher rpm's, right? > Well, with this prop I first set it up turning 6200 rpm's on the > ground and > took it up for a test flight. Max level flight rpm's was about 5700~5800 > rpm's and the engine was real slow to rev up. This scared me for > a minute or > two as I thought something was going wrong with the engine. > I then went back and adjusted the prop twice more and wound up with 6600 > static and 6400 WOT level flight. > This prop came off a Firestar and supposedly vibrated real bad > and this was > the reason for selling. I fixed the vibration problem, but am > puzzled by the > lower rpm's in WOT level flight. The climb rate seems about normal but I > really couldn't tell as it was very bumpy yesterday. My butt came > out of the > seat a few times while descending for landings. > I have heard of constant speed blades on Warp drive props. Is > this possibly > the reason for the lower flight rpm's I am seeing? > > Thanks, > John Cooley > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Prop noise
Date: Nov 27, 2005
| that I had raised it. But the sound difference was noticeable. The | bolts are long enough to go up 3/4 inch, so I will try that. | | John Jung John J/Gang: Let me ask you a question. In the process of raising the thrust line to reduce noise, are we also reducing performance? john h MKIII Titus, Alabama ________________________________________________________________________________
From: "Richard & Martha Neilsen" <NeilsenRM05(at)comcast.net>
Subject: Re: Prop noise
Date: Nov 27, 2005
John/All You would think that raising the trust line would decrease performance but I don't see it. I had 7 inches of clearance between the boom tube and the tips of my 72 inch prop with my old engine mount. Now with the lower engine mount I have app 1.75 inch clearance. This is likely much more than most people would move their thrust line but I had no detectable change in performance. With that said I did have some very undesirable handling issues with the high thrust line but again most people will not likely move their thrust line up as high as I did. In my own defense I didn't just create that high thrust line for the heck of it. The VW engine with the Valley reduction drive just didn't allow a lower mounting with the stock Kolb cage/engine mount. Rick Neilsen Redrive VW powered MKIIIc ----- Original Message ----- From: "John Hauck" <jhauck(at)elmore.rr.com> Subject: Re: Kolb-List: Prop noise > > > | that I had raised it. But the sound difference was noticeable. The > | bolts are long enough to go up 3/4 inch, so I will try that. > | > | John Jung > > John J/Gang: > > Let me ask you a question. > > In the process of raising the thrust line to reduce noise, are we also > reducing performance? > > john h > MKIII > Titus, Alabama ________________________________________________________________________________
Date: Nov 27, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Re: Warp Drive prop question
What engine/gearbox combination do you have that prop on? Years ago I had an Anglin J-6 with a 503 on it and a 66" Warp Drive 2 blade, and I had exactly the same situation. I had to prop it for a high static rpm because as I began my takeoff roll, the prop would load up and the RPM's would decrease. It acted exactly as if the prop were stalled at static rpm, and was revved a bit higher than you would expect - and then unstalled and loaded up and slowed down as the takeoff roll began - which actually makes sense, because a 2 blade prop will have a higher angle of attack (more pitch) than a three blade prop for a given horsepower and prop diameter, and might have had too much pitch for realistic results at a static runup. But as soon as forward speed increases at takeoff, the blade unstalls and loads up the prop, and the engine slows down. I have my MKIII/582 propped for about 64-6500 WOT, so it sounds like you are currently in the ball park, even though you got there by non standard means. Richard Pike MKIII N420P (420ldPoops) > >Hi Guys, >Got a question for you Warp Drive folks or anyone that can enlighten me. I >bought a 66" 2 blade taper tip prop for my MK II that I have been sprucing >up to sale. I didn't like the GSC prop that was on it is the reason for >switching. Anyhow back to the question. With the GSC and the Powerfin prop >on my FS II I would always set the prop for about 6200~6300 static rpm's to >achieve the 6600~6700 level flight WOT rpm's. The prop unloads in flight and >turns higher rpm's, right? >Well, with this prop I first set it up turning 6200 rpm's on the ground and >took it up for a test flight. Max level flight rpm's was about 5700~5800 >rpm's and the engine was real slow to rev up. This scared me for a minute or >two as I thought something was going wrong with the engine. >I then went back and adjusted the prop twice more and wound up with 6600 >static and 6400 WOT level flight. >This prop came off a Firestar and supposedly vibrated real bad and this was >the reason for selling. I fixed the vibration problem, but am puzzled by the >lower rpm's in WOT level flight. The climb rate seems about normal but I >really couldn't tell as it was very bumpy yesterday. My butt came out of the >seat a few times while descending for landings. >I have heard of constant speed blades on Warp drive props. Is this possibly >the reason for the lower flight rpm's I am seeing? > >Thanks, >John Cooley > > >-- > > ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 27, 2005
Subject: MKlllx Speed
For those that are interested I made some speed runs today as conditions were decent. It got to about 45-50 degrees today and I was able to consistently get 1000 FPM climb on repeated take offs. That was with 6500 RPM and 58-60 MPH indicated. I made a couple of runs where I kept inching up the throttle and arrived at 84 MPH indicated turning 6500 RPM. I'm finding 5000 RPM is a comfortable cruise setting and seems to be somewhat fuel efficient. Read a couple of posts concerning the loading/unloading of props. I'm turning a 66" Warp 3 Blade With taper and do not see any difference at WOT on the ground or in the air (6500 RPM). However, I will watch closer from now on. Larry Tasker MKlllx 582 3-blade warp ________________________________________________________________________________
From: "John Cooley" <johnc(at)datasync.com>
Subject: Warp Drive prop question
Date: Nov 28, 2005
Richard, It's a 503 DCDI with a 2.58 "B" box. The first MK II Twinstar that I owned had the same engine combo and a 3 blade taper tip Warp Drive on it. I never fooled with the pitch setting on it but as best I remember it performed real well. My other experiences are with a 3 blade Powerfin and 2 blade GSC and both of these have to be set several hundred RPM lower static to achieve the max rpm WOT in level flight. Where do you start with the IVO's? Later, John Cooley -----Original Message----- From: owner-kolb-list-server(at)matronics.com [mailto:owner-kolb-list-server(at)matronics.com] On Behalf Of Richard Pike Subject: Re: Kolb-List: Warp Drive prop question What engine/gearbox combination do you have that prop on? Years ago I had an Anglin J-6 with a 503 on it and a 66" Warp Drive 2 blade, and I had exactly the same situation. I had to prop it for a high static rpm because as I began my takeoff roll, the prop would load up and the RPM's would decrease. It acted exactly as if the prop were stalled at static rpm, and was revved a bit higher than you would expect - and then unstalled and loaded up and slowed down as the takeoff roll began - which actually makes sense, because a 2 blade prop will have a higher angle of attack (more pitch) than a three blade prop for a given horsepower and prop diameter, and might have had too much pitch for realistic results at a static runup. But as soon as forward speed increases at takeoff, the blade unstalls and loads up the prop, and the engine slows down. I have my MKIII/582 propped for about 64-6500 WOT, so it sounds like you are currently in the ball park, even though you got there by non standard means. Richard Pike MKIII N420P (420ldPoops) -- ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop noise
Date: Nov 28, 2005
John H. and Group, I think Rick Neilsen may have already answered this, but no, I didn't notice any change in performance or handling. John Jung Firestar II N6163J Surprise, AZ On Nov 28, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > > | bolts are long enough to go up 3/4 inch, so I will try that. > | > | John Jung > > John J/Gang: > > Let me ask you a question. > > In the process of raising the thrust line to reduce noise, are we also > reducing performance? ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop noise
Date: Nov 28, 2005
jerb and Group, The IVO on my Firestar II has the spacer and it does make a big difference in lowering the noise. The Firestar II was designed with the engine farther forward that the original Firestar, causing this problem. When I started flying the II, I had wanted to use my taper tip 66" Warp from my original Firestar. But on first try, the noise was terrible. I would have added the spacer to the Warp, but it is too heavy to be on a B box with a spacer. This is the only reason that I run an IVO instead or a Warp. John Jung Firestar II N6163J Surprise, AZ On Nov 27, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > When I was at Oshkosh back in 95 looking at the FireFly, Dennis > commented about the noise being generated by the prop passing the > trailing edge of the wing, they added a spacer to increase the > clearance and found it reduced the noise also. John Hack might know > more about this. > jerb ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: warp prop
Date: Nov 28, 2005
| Listers, thanks for the observations on the warp prop characteristics | regarding static to inflight WOT. | -BB | BB/Gang: I'm probably confused, but I understand there is a lot of difference between static rpm, WOT climb rpm, and WOT straight and level flight rpm. The way I prop my airplanes, no matter what prop I am using, whether it is an Ultrastar, Firestar, or MKIII (I don't like to put a "c" behind MKIII. My MKIIII was here long before the Xtra came along), is adjust the prop so I can turn the red line at WOT straight and level flight, not WOT in a climb attitude. Initially, static rpm is only a starting point in adjusting my prop to my engine and airplane. What determines what the final pitch adjustment is going to be, whether two or four stroke, or what ever model Kolb I am flying, is WOT straight and level flight with the tachometer indicating the engine is just touching the red line. If I do it that way I get the best climb and cruise performance. I am also loading and operating the engine the way the designers intended it to be operated. Once I get the prop pitched so that the engine is turning red line rpm, in my case 5,500 rpm, with the throttle wide open and the aircraft in straight and level flight, I am set to go. I can then get the correct static rpm next time I am on the ground to use during my pretakeoff check. With a 72" 3 blade taper tip Warp Drive Prop on a 912ULS I get the following characteristics: 1) A drop of approximately 100 to 150 rpm from static rpm soon after the MKIII starts its take off roll. 2) It holds that rpm through climb out at 60 to 70 mph indicated air speed. 3) If I keep the throttle wide open in a straight and level attitude the engine will turn the red line rpm, 5,500, and no more, unless I put the nose down. To me, the most important indicator for proper pitch setting is bumping the redline with the engine at WOT and in straight and level flight. That dictates all the other rpm readings, static and climb and cruise. Overpitching a prop to keep rpm's lower to save the engine is probably more harmful than not having enough pitch. I think a realistic comparison of an overpitched prop and overloaded engine is driving a 5 speed automobile around in 5th gear all the time. In the airplane's situation, with an overpitched prop, it is like operating that automobile in a gear, too high, while continuously climbing a steep hill. This is actually overworking the engine and not saving it, in my humble opinion. These engines were meant to be turned and they operate best at about 75% power, or 5,800 rpm for the Rotax two strokes, and 5,000 rpm for the 912 series four strokes. These engines are designed and tuned to be continuous duty engines, not motor cycles, weed eaters, or automobiles. Better stop now. I am confusing myself even more. hehehe john h MKIII Titus, Alabama ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: hello?
Date: Nov 28, 2005
1.76 SUB_HELLO Subject starts with "Hello" Please ignore, testing... LS N646F ________________________________________________________________________________
Date: Nov 28, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Fine Tuning the Bing 54 for the Victor 1+
Kolbers, I know not many are flying with Victor 1 engines, but the following information may be helpful. If I knew then what I know now, I might still be flying with a Rotax engine. Moving has kept me from flying as much as I would like, but having the FireFly closer has let me experiment a little more. And I have been concentrating on getting the engine to run well at all engine speeds. The basic problem with the Victor 1+ is that it uses the Bing 54 carburetor. The carburetor is much too large for the engine. This makes it more sensitive to adjust because the engine will run at full power with the throttle at less than 30% open position. First, I worked on fuel flow variation. I could fly twice in the same day, at the same altitude, temperature, and rpm, and experience several 0.1s of a gallon in fuel flow. I found that by purchasing and installing a strong throttle return spring from Bing, that this variation was reduced to 0.01s of a gallon. Also the reduction of needle bounce lead to a reduction in fuel flow. Bing ships all carburetors with the middle strength spring. I recommend replacing them with the strongest spring. Second, I worked on improving engine idle and low speed performance. I installed a 25 idle jet and EGT's at the non flight engine speeds increased and the engine does not quit on final. This change created a problem, in that, the EGT would exceed the upper limit if the engine was operated between 5,000 and 6,000 rpm. The above lead to checking out the needle and needle modification. Although this effort may not be complete, the engine can be operated through the complete operating range without exceeding the EGT limit with improved fuel flow rates. If you would like to see how it was done, it can be found at: http://www.thirdshift.com/jack/firefly/firefly121.html The most difficult part of this project was to come up with gauge that lets one accurately determine needle position relative to throttle opening. If you would like a copy of the gauge, let me know. If you have a Dermel tool, a micrometer, and a small flat file, you can modify a needle. Others have said that one should believe the plugs. In the past I have put too much faith in the EGT gauge, and so I would stop dropping the needle if the temperature reached 1,250 degrees F. But by reading the plugs and dropping the needle by one-quarter of a slot at a time, I discovered the EGT does not always continue to increase. The EGT temperature held steady, and fuel consumption went down. At this time the plugs are indicating rich, so when the weather improves, I will start dropping the needle again by one-quarter of a slot at a time. I did install a second EGT probe down stream about six inches from the original probe. It mirrors the original probe temperatures up through about 4,000 rpm. At this point the down stream probe increases and reads higher. Through the cruise rpm region it reads 100 degrees higher than the original probe. This gives more credence to reading the plugs. To save weight, I will be removing the down stream probe. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
Date: Nov 28, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Kolb Hauling...
SSdtIHBsYW5uaW5nIHRvIGhhdWwgYSBmb2xkZWQgd2luZ3MgRmlyZXN0YXIgNzcwIG1pbGVzIHRo aXMgbW9udGguLi4gIEknbGwKYmUgdXNpbmcgYSBmbGF0YmVkIHRyYWlsZXIuLi4gIEFueSB3b3Jk cyBvZiB3aXNkb20/Li4uCgotLQr0v/QKCldoYXQgZnJlZWRvbSBsaWVzIGluIGZseWluZywgd2hh dCBHb2RsaWtlIHBvd2VyIGl0IGdpdmVzIHRvIG1lbi4uLiBJIGxvc2UKYWxsIGNvbnNjaW91c25l c3MgaW4gdGhpcyBzdHJvbmcgdW5tb3J0YWwgc3BhY2UgY3Jvd2RlZCB3aXRoIGJlYXV0eSwgcGll cmNlZAp3aXRoIGRhbmdlci4uLgoKlyBDaGFybGVzIEEuIExpbmRiZXJnaAoKZG8gbm90IGFyY2hp dmUK ________________________________________________________________________________
From: "Don Gherardini" <donghe@one-eleven.net>
Subject: Re: warp prop
Date: Nov 28, 2005
John, That is a pretty good description of how a fella ought to treat any engine. The method of useing a load to limit an engines rpms is certainly not the same thing as simply lowering the throttle setting to limit the rpms. Alot of people dont understand the difference and think an engine LOADED to , say, 75% of max recommended rpms is the same as reducing the throttle to 75% of rpms...IT is certainly not. WHen we load the engine to 75% of the rpms we have effectively OVERLOADED the design limits of the engine, and it is much more strenuous on the engine. So Gentleman, adjust your props to load your engines as John has described, and when flying, reduce the throttle to run at the rpms you desire, this way instead of increaseing it, and your engine will last a whole lot longer. Don Gherardini OEM.Sales / Engineering dept. American Honda Engines Power Equipment Company CortLand, Illinois 800-626-7326 ________________________________________________________________________________
From: N27SB(at)aol.com
Date: Nov 28, 2005
Subject: Re: Kolb Hauling...
In a message dated 11/28/05 11:48:28 AM Central Standard Time, david(at)davidlehman.net writes: > > I'm planning to haul a folded wings Firestar 770 miles this month... I'll > be using a flatbed trailer... Any words of wisdom?... > > Thanx... > > David > Hi David, I am currently hauling my Firefly on Floats on an open trailer. I played around with several configurations and some worked better than others. The airplane really likes to be hauled moving beak to the wind. In my case I had to come up with a solution that was solid and stable as well as quick to load and unload. I would be happy to send you some pictures of what I did. BTW, I have a real nice enclosed Firefly trailer that my Firefly does not fit in due to the floats. I need to sell it but I do not think it is long enough for you. Steve B ________________________________________________________________________________
Date: Nov 28, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Kolb Hauling...
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From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: new member and Q's on Mark III Xtra
Date: Nov 28, 2005
Hello all, New Kolb list member here. I'm currently the proud of owner of a Firestar II (N646F) that was expertly built by a fellow name of Dale Atchetee in Victoria, TX. I have about 50 hours in it so far and love it already. I like this plane so much, in fact, I've given some thought to eventually replacing it (or supplementing it) with a Mark III Xtra. I'd like something just like my FSII, but a bit bigger/heavier that'll handle wind a bit better. That's about the only mission objective my FSII isn't that wonderful for. So I'm looking at the Mark III Xtra as a possibl future replacement. Everything else - the view, quality of build, folding wings, and so on, are pretty much met. A little extra cruise speed would be nice too. So, my specific questions are: - Does anyone have experience with the quickbuild kits currently produced by Kolb? I likely would go the quickbuild route for time reasons. - Kolb themselves - how is the current company to deal with as far as service, parts, quality of the build manuals and so on? - Any other general statements to make about the Mark III Xtra? I like the Mark III classic also, but Xtra has the additional cruise speed which looks nice to have. thanks for any input you may have, LS N646F ________________________________________________________________________________
Date: Nov 28, 2005
From: bryan green <lgreen1(at)sc.rr.com>
Subject: Re: new member and Q's on Mark III Xtra
lucien stavenhagen wrote: > >Hello all, > > I can't comment on the extra other than I would like to have one also, but for Travis and the guys at TNK you could not ask for a better bunch of folks to work with. They go out of their way to be as helpful as possible. Bryan Green Elgin SC Firestar 447 BRS > > >- Kolb themselves - how is the current company to deal with as far as >service, parts, quality of the build manuals and so on? > >- Any other general statements to make about the Mark III Xtra? > > > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: new member and Q's on Mark III Xtra
Date: Nov 28, 2005
Lucien/Gang: | - Does anyone have experience with the quickbuild kits currently produced by | Kolb? I likely would go the quickbuild route for time reasons. Don't think you will find a better quick build deal anywhere. | - Kolb themselves - how is the current company to deal with as far as | service, parts, quality of the build manuals and so on? Won't find a better company or people to deal with. They are there to help the customer any way they can, as long as customers do not abuse their help. john h MKIII Titus, AL ________________________________________________________________________________
From: "Jim Ballenger" <ulpilot(at)cavtel.net>
Subject: Re: new member and Q's on Mark III Xtra
Date: Nov 28, 2005
LS The Kolb folks are just great to do business with. Over the 2 1/2 years I was building my MK III X they always had time to answer my questions on building or flying the X or if I just wanted to talk in general. If I needed the missing bolt or hardware I would call them up and it would be on it's way that day. I never doubted that what they said they would do would not get done. I am extremely satisfied with my X. I decided on the X over the standard model because I could keep my feet in front of me, not angled and I liked the instrument panel placement better on the X. I had a FS KXP while building the X and enjoyed flying it. The reason I wanted the X was to take the occasional passenger up and share my passion for grass root flying. It's a great plane but it still has a light wing load to it. Jim Ballenger MK III X 582 Virginia Beach, VA ----- Original Message ----- From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com> Subject: Kolb-List: new member and Q's on Mark III Xtra > > > Hello all, > New Kolb list member here. I'm currently the proud of owner of a Firestar > II > (N646F) that was expertly built by a fellow name of Dale Atchetee in > Victoria, TX. I have about 50 hours in it so far and love it already. > > I like this plane so much, in fact, I've given some thought to eventually > replacing it (or supplementing it) with a Mark III Xtra. I'd like > something > just like my FSII, but a bit bigger/heavier that'll handle wind a bit > better. That's about the only mission objective my FSII isn't that > wonderful > for. So I'm looking at the Mark III Xtra as a possibl future replacement. > Everything else - the view, quality of build, folding wings, and so on, > are > pretty much met. A little extra cruise speed would be nice too. > > So, my specific questions are: > > - Does anyone have experience with the quickbuild kits currently produced > by > Kolb? I likely would go the quickbuild route for time reasons. > > - Kolb themselves - how is the current company to deal with as far as > service, parts, quality of the build manuals and so on? > > - Any other general statements to make about the Mark III Xtra? > > I like the Mark III classic also, but Xtra has the additional cruise speed > which looks nice to have. > > thanks for any input you may have, > > LS > N646F > > > ________________________________________________________________________________
From: Cat36Fly(at)aol.com
Date: Nov 28, 2005
Subject: Re: MKlllx Speed
Jim; That seems like a heck of a lot of loss for an atmospheric change. The air has been somewhat the same a couple hundred miles north (Delaware) and I'm running the best ever (per my last post). I'm a beginner with these two cycles but a 50% drop due to density? Out of curiosity, why the plug swap? I'm guessing you have 50+ hours on those! Larry Tasker MKlllx 582 ________________________________________________________________________________
From: "dama" <dama(at)mindspring.com>
Subject: Re: 503 de-carbon
Date: Nov 28, 2005
John, I am at 260 hours with no de-carbon jobs yet. At 150 hours I took it to a mechanic for service and he said there was no need to tear into it. At 300, I plan to overhaul it and I'm curious to see how it looks inside. BTW, I run Pennzoil air cooled with a dash of Marvels... Kip ----- Original Message ----- From: "John Jung" <jrjungjr(at)yahoo.com> Subject: Kolb-List: 503 de-carbon > > Group, > > Recently, I pulled the exhaust from my 503 to check for carbon. I had > 100 hours since my last de-carbon. I have never been able to get a good > feeling from checking through the exhaust port, and this time was no > exception, so I took the engine off and pulled the heads and cylinders. > I found one oil ring stuck on an end and the other oil ring had a 3/8" > piece broke off the end. I have no idea what caused the ring to break > or how long it had been that way, but I was glad that I decided to do a > complete check. > > As far as the stuck ring goes, is this normal after only 100 hours? > After my last de-carbon, I switched to oil injection and Pennsoil air > cooled. Also, I try to keep the rpm's and temps up to avoid carbon. All > I can think of is that maybe I didn't remove enough carbon from the > ring lands last time. I used to use Amsoil and the carbon from that oil > is really hard. > > I always feel better about flying after I have seen the pistons and > cylinders. Carbon may be a concern for me but wear isn't. The rings and > cylinders measured well within new specs after 200 hours. > > John Jung > Firestar II N6163J > Surprise, AZ > > ________________________________________________________________________________
Date: Nov 28, 2005
From: "David L. Bigelow" <dlbigelow(at)verizon.net>
Subject: Warp Drive prop question
Interesting characteristic of Warp Drive props. Every prop I've ever used (quite a few) has required static setting of pitch to result in a WOT rpm of 200-300 below maximum rpm on the ground. In flight at WOT, you get the maximum RPM - the faster you go, the higher the RPM. That's the case with my FS2 equipped Rotax 503 with a 66 inch Powerfin prop. I set it statically for 6200 rpm, and get 6400-6500 rpm in flight at WOT. > The prop unloads in flight and > turns higher rpm's, right? > Well, with this prop I first set it up turning 6200 rpm's on the ground and > took it up for a test flight. Max level flight rpm's was about 5700~5800 > rpm's Dave Bigelow Kamuela, Hawaii FS2 Rotax 503 ________________________________________________________________________________
From: "Don Gherardini" <donghe@one-eleven.net>
Subject: Re: warp prop
Date: Nov 28, 2005
Gentlemen...and ladies... I ought proof-read my posts a little better...sorry about the confusing verbage at the end of my last post...I typed: "..that way , instead of increasing it, your engine will last...."" I was sitting at my desk reading the Kolb list stuff...(supposed to be working) and, well...I cut the post short when I was distracted (by work) and didn't make a bit of sense with the last sentence....aright.... my apologies to all! What I was thinking ...and didnt get transfered from my brain to the keyboard...was : Instead of increaseing BMEP.. (brake mean effective pressure) or cylinder pressure, from an overloaded condition, you will decrease it and your engine will last alot longer at the same rpm level. Another benefit of cruiseing at the rpm level where the BMEP is the highest..(which will be the peak torque rpm) is that the most horsepower will be delivered for the fuel burned, because the engine is at its most efficient cylinder filling capacity. The efficiency level always corresponds very closely to the peak torque rpm point on the performance curve. To acheive the level of efficiency the load vs power produced must be co-ordinated with the throttle opening for the best breathing for any given rpm, and it will certainly not be co-ordinated correctly unless the WOT position of the fuel delivery system (carbs in this case) is at the max rpm point. IF the max rpm level is reduced at WOT due to a heavier load than the power produced can compensate for, the efficiency goes down quickly. Many other detrimental things also happen. such as: Heat cannot be dispersed effectively, Percent of Fuel burned in combustion drops, Carbon buildup due to unburned residues, Oil varnish on piston walls increases, Pre-detonation occours when cylinder pressures get high enough for particular conditions, Connecting Rod stress increases at an alarming rate, and so on. Another thing that happens is our performance curve is no longer valid.....that right....if we have a 65 horse engine at 6600 rpms.....the load applied must let the engine turn 6600 rpms when the throttle is wide open. If the throttle is wide open and the engine will not turn 6600 rpms due to the load...then the load will NOT let the engine produce 55 horsepower at 5500 rpms because the throttle opening will not be correct for the correct amount of fuel and air to be delivered. CV carbs compensate for this somewhat....but they are always behind the curve because manifold vacuum will always be off according to the power produced. About all they really do is keep the speed of the mixture flowing thru the carb fast enough to keep fuel coming thru the main jet at a little more accurate rate according to the air the engine is pumping thru itself. I Hope I am better explaining myself tonite.....whew.....I did proof-read this one...which still doesnt insure its accuracy!!!! Ya never know, I Could be I am all wrong about all this stuff! Don Gherardini FireFly 098 http://www.geocities.com/dagger369th/my_firefly.htm ________________________________________________________________________________
From: "David Key" <dhkey(at)msn.com>
Subject: Mark III Extra build time
Date: Nov 28, 2005
Hi guys. What's the build time on a Mark III Extra with the quick build option? I had a Mark III classic a few years ago. Now, after getting my instrument rating and buying a house on an airport, I've decided that I liked flying that Kolb way more than jacking with instruments and filing flight plans. I've got to get out from behind that instrument panel. I miss my Kolb, I should wait a year and buy someone's xtra just thought I'd look at buiding one if it isn't too hard. ________________________________________________________________________________
Date: Nov 29, 2005
Subject: Wiring diagram
From: rap(at)isp.com
As the wiring diagram says it is a work in progress.I still have not determined the cicuit breaker req'd for the started soleniod. And I'm not real sure about my wiring of the rectifier. Rick Pearce Mark3C amphib DO NOT ARCHIEVE ----------------------------------------- ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Re: new member and Q's on Mark III Xtra
Date: Nov 29, 2005
Hey Jim, Ok, thanks for the info. Yeah I remember the original builder of my FSII complained about the kit a bit, that it was disorganized and etc. Looking through the builders manual supplied with it, it wasn't, er, exactly builder-friendly.. ;) But this one is a 96 model, and I assume the new company has upgraded the manuals and probably made improvements to the kits. That's what I've heard anyway... Speaking of that, how are the builders manuals, plans, etc.? Pretty well laid out? Any confusing parts? Just wondering how that part of building is... Thanks, LS >LS > >The Kolb folks are just great to do business with. Over the 2 1/2 years I >was building my MK III X they always had time to answer my questions on >building or flying the X or if I just wanted to talk in general. If I >needed the missing bolt or hardware I would call them up and it would be on >it's way that day. I never doubted that what they said they would do would >not get done. > >I am extremely satisfied with my X. I decided on the X over the standard >model because I could keep my feet in front of me, not angled and I liked >the instrument panel placement better on the X. I had a FS KXP while >building the X and enjoyed flying it. The reason I wanted the X was to >take >the occasional passenger up and share my passion for grass root flying. >It's a great plane but it still has a light wing load to it. > >Jim Ballenger >MK III X 582 >Virginia Beach, VA > > >----- Original Message ----- >From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com> >To: >Subject: Kolb-List: new member and Q's on Mark III Xtra > > > > > > > > Hello all, > > New Kolb list member here. I'm currently the proud of owner of a >Firestar > > II > > (N646F) that was expertly built by a fellow name of Dale Atchetee in > > Victoria, TX. I have about 50 hours in it so far and love it already. > > > > I like this plane so much, in fact, I've given some thought to >eventually > > replacing it (or supplementing it) with a Mark III Xtra. I'd like > > something > > just like my FSII, but a bit bigger/heavier that'll handle wind a bit > > better. That's about the only mission objective my FSII isn't that > > wonderful > > for. So I'm looking at the Mark III Xtra as a possibl future >replacement. > > Everything else - the view, quality of build, folding wings, and so on, > > are > > pretty much met. A little extra cruise speed would be nice too. > > > > So, my specific questions are: > > > > - Does anyone have experience with the quickbuild kits currently >produced > > by > > Kolb? I likely would go the quickbuild route for time reasons. > > > > - Kolb themselves - how is the current company to deal with as far as > > service, parts, quality of the build manuals and so on? > > > > - Any other general statements to make about the Mark III Xtra? > > > > I like the Mark III classic also, but Xtra has the additional cruise >speed > > which looks nice to have. > > > > thanks for any input you may have, > > > > LS > > N646F > > > > > > > > ________________________________________________________________________________
Date: Nov 30, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Kolb Hauling...
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From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Kolb Hauling...
Date: Nov 30, 2005
David L/Gang: Maybe..............if you change your email from HTML to Plaintext, your posts will come out on the Kolb List so we can all understand what you are trying to communicate. If that is not the problem, maybe Matte or someone else has some help to get your problem squared away. Take care, john h MKIII titus, alabama Subject: Re: Kolb-List: Kolb Hauling... | | VGhhbnggR2VvcmdlLi4uCgpJIHRvbyBhbSBjb25jZXJuZWQgYWJvdXQgdGhlIGNyb3Nzd2luZCBz ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Nov 30, 2005
Subject: Re: Wiring diagram
In a message dated 11/29/2005 1:20:02 P.M. Eastern Standard Time, rap(at)isp.com writes: --> Kolb-List message posted by: rap(at)isp.com As the wiring diagram says it is a work in progress.I still have not determined the cicuit breaker req'd for the started soleniod. And I'm not real sure about my wiring of the rectifier. Rick Pearce Mark3C amphib on the rectifier, just make sure the ac side is not grounded with the dc side....otherwise it will blow the bridge George Randolph Firestar driver from The Villages, Fl Rotax 447, 3 blade Ivo, KX, 1991 ________________________________________________________________________________
From: Kirby Dennis Contr MDA/AL <Dennis.Kirby(at)kirtland.af.mil>
Subject: New Memeber Q's on Mark III
Date: Nov 30, 2005
<< Kolb themselves - how is the current company to deal with as far as service, parts, quality of the build manuals and so on? >> Lucien, and fellow Kolbers - Here's my answer: This summer, I installed a Rotax-912ul on my Mark-III. To do this, I had to order a 912 Installation Kit from the Kolb factory ($850.) I called Travis at TNK and told him I needed the kit, but at that price, I'd have to save up for a few weeks and therefore, would not be ordering it for another month or so. Three days later, the kit shows up on my doorstep with a note from Travis saying, "Here's the Kit - get started on your installation. Send us a check when you can." How many companies provide THAT kind of customer support? I rest my case. Dennis Kirby Mark-III, 912ul, in Cedar Crest, New Mexico ________________________________________________________________________________
From: Kirby Dennis Contr MDA/AL <Dennis.Kirby(at)kirtland.af.mil>
Subject: Re: Kolb Hauling...
Date: Nov 30, 2005
<<... Any words of wisdom? ... Thanx >> David - I, too, use a flatbed trailer to transport my Mark-III. Here is my idea for supporting the tail: http://www.matronics.com/photoshare/Dennis.Kirby@kirtland.af.mil.02.12.2005/ <http://www.matronics.com/photoshare/Dennis.Kirby@kirtland.af.mil.02.12.2005 /> Once on the trailer, I set an old tire under the dolly for added shock absorption. The whole affair is then securely strapped down. Works great. Dennis Kirby New Mexico ________________________________________________________________________________
From: "Denny Rowe" <rowedl(at)highstream.net>
Subject: Hauling Kolbs on flat beds
Date: Nov 30, 2005
You may also consider removing the wings and laying them flat on the trailer deck to reduce side area. If you are pulling with a truck that has a cap, or a van, one of the wings can even be strapped to the roof. With the bird exposed you really get a lot of wind loads on the folded structure that it is not meant to take. Also dont forget to make control locks for the tail feathers, I made mine out of CPVC pipe with pipe foam insulation over them for padding. You need four TEEs and four elbows in addition to the pipe. Denny Rowe, Mk-3 PA ________________________________________________________________________________
Date: Nov 30, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Kolb Hauling...
Dennis, more great ideas and I appreciate the pictures, thanx... David On 11/30/05, Kirby Dennis Contr MDA/AL wrote: > > Dennis.Kirby(at)kirtland.af.mil> > > <<... Any words of wisdom? ... Thanx >> > > > David - > > > I, too, use a flatbed trailer to transport my Mark-III. > > Here is my idea for supporting the tail: > > > http://www.matronics.com/photoshare/Dennis.Kirby@kirtland.af.mil.02.12.2005/ > < > http://www.matronics.com/photoshare/Dennis.Kirby@kirtland.af.mil.02.12.2005 > /> > > > Once on the trailer, I set an old tire under the dolly for added shock > absorption. > > The whole affair is then securely strapped down. > > Works great. > > > Dennis Kirby > > New Mexico > > ________________________________________________________________________________
Date: Nov 30, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Hauling Kolbs on flat beds
Thanx Denny, I've been considering the "wing removed" option too... I noticed the tail lock in some of the pictures on the net... How long do the pieces of pipe need to be?... Unfortunately, I don't have a Kolb locally to look at, so I'm going to have to prepare everything before I go to pick it up... Thanx again... David On 11/30/05, Denny Rowe wrote: > > > You may also consider removing the wings and laying them flat on the > trailer deck to reduce side area. > If you are pulling with a truck that has a cap, or a van, one of the wings > can even be strapped to the roof. > With the bird exposed you really get a lot of wind loads on the folded > structure that it is not meant to take. > Also dont forget to make control locks for the tail feathers, I made mine > out of CPVC pipe with pipe foam insulation over them for padding. You need > four TEEs and four elbows in addition to the pipe. > > Denny Rowe, Mk-3 PA > ________________________________________________________________________________
Date: Nov 30, 2005
From: ray anderson <rsanoa(at)yahoo.com>
Subject: Re: Hauling Kolbs on flat beds
My Kolb Ultra Star was transported about 800 miles about one year ago on a flat bed trailer. The wings were removed and stacked underneath the fuselage with a light wood frame between them to keep them apart. Every thing was wrapped in a commercial grade plastic similar to Saran Wrap. Careful planing and wrapping will insure there is no gap that will permit wind to get in between any sections of the structure. The wrap is available at most hardware stores and Lowes and comes in a large roll about two feet in width. Is quite cheap. Movers blankets were wrapped across corners and pointy areas before the plastic wrap. The rear of the fuselage should be supported in some manner so the aircraft doesn't rest on the tail wheel. Lash every thing down securely and there should be no problem. I would strongly suggest that you don't haul it with wings folded. You can encounter some pretty strong unexpected side loadings in a long haul like that. Could even tilt the trailer. Thanx Denny, I've been considering the "wing removed" option too... I noticed the tail lock in some of the pictures on the net... How long do the pieces of pipe need to be?... Unfortunately, I don't have a Kolb locally to look at, so I'm going to have to prepare everything before I go to pick it up... Thanx again... David On 11/30/05, Denny Rowe wrote: > > > You may also consider removing the wings and laying them flat on the > trailer deck to reduce side area. > If you are pulling with a truck that has a cap, or a van, one of the wings > can even be strapped to the roof. > With the bird exposed you really get a lot of wind loads on the folded > structure that it is not meant to take. > Also dont forget to make control locks for the tail feathers, I made mine > out of CPVC pipe with pipe foam insulation over them for padding. You need > four TEEs and four elbows in addition to the pipe. > > Denny Rowe, Mk-3 PA > --------------------------------- Single? There's someone we'd like you to meet. ________________________________________________________________________________
From: "Michael Bigelow" <orcabonita(at)hotmail.com>
Subject: New Memeber Q's on Mark III
Date: Nov 30, 2005
I decided on the Kolb MK III Xtra due to its flying qualities and design above all else, that is what is most important to me. That being said..... Now that I having the Mark III built, and the Kolb company has been awesome. They are very responsive and helpful, and Travis does everything possible to make whatever I need happen. You could not deal with a better, more honest and hard working bunch of people. A really good product backed by a great bunch of people, it just does not get any better than that !!!! Mike Bigelow ________________________________________________________________________________
From: "Bob and Jenn B" <tabberdd(at)hotmail.com>
Subject: Trailering
Date: Dec 01, 2005
Another suggestion would be to rent a U-haul and fit it all inside or call Andy Haaden, his number is on Barnstormers / Services, who runs an aircraft delivery service. He brought mine home last year at $1.25 loaded mile (that was before the gas increases). Takes care of everything and is cheaper than breaking the plane on the way. Bob ________________________________________________________________________________
Date: Dec 01, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Trailering
Thanx Bob... Those are two more thoughts I also had... I'm combining a family Christmas trip with the airplane pickup... I just bought a new Diesel Ford 4X4 pickup and I'm guessing my chances of good road traction are better with the pickup than an Uhaul truck during the Winter... I'm getting some real good information here and I'm leaning towards removing the wings and wrapping it up like a Christmas present... David On 12/1/05, Bob and Jenn B wrote: > > > Another suggestion would be to rent a U-haul and fit it all inside or call > Andy Haaden, his number is on Barnstormers / Services, who runs an > aircraft > delivery service. He brought mine home last year at $1.25 loaded mile > (that > was before the gas increases). Takes care of everything and is cheaper > than > breaking the plane on the way. > > Bob > ________________________________________________________________________________
Date: Dec 01, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Hauling Kolbs on flat beds
Thanx Ray, how you doing?... David On 11/30/05, ray anderson wrote: > > > My Kolb Ultra Star was transported about 800 miles about one year ago on a > flat bed trailer. The wings were removed and stacked underneath the fuselage > with a light wood frame between them to keep them apart. Every thing was > wrapped in a commercial grade plastic similar to Saran Wrap. Careful planing > and wrapping will insure there is no gap that will permit wind to get in > between any sections of the structure. The wrap is available at most > hardware stores and Lowes and comes in a large roll about two feet in > width. Is quite cheap. Movers blankets were wrapped across corners and > pointy areas before the plastic wrap. The rear of the fuselage should be > supported in some manner so the aircraft doesn't rest on the tail wheel. > Lash every thing down securely and there should be no problem. I would > strongly suggest that you don't haul it with wings folded. You can encounter > some pretty strong unexpected side loadings in a long haul like that. Could > even tilt the trailer. > ________________________________________________________________________________
Date: Dec 01, 2005
From: Mike Pierzina <planecrazzzy(at)yahoo.com>
Subject: RE:FSII / Control Stick-New & OLD
It's in the Matronics Photoshare http://www.matronics.com/photoshare/planecrazzzy@lycos.com.02.15.2004/ You were looking for a view on a aileron gap seal....I think that's at "Kip's" site......? --------------------------------- ________________________________________________________________________________
Date: Dec 01, 2005
From: possums <possums(at)mindspring.com>
Subject: Re: 503 de-carbon
At 07:33 PM 11/28/2005, you wrote: > >John, I am at 260 hours with no de-carbon jobs yet. At 150 hours I took it >to a mechanic for service and he said there was no need to tear into it. At >300, I plan to overhaul it and I'm curious to see how it looks inside. Me too - got 669 hours now without a decarb - really. 1999 Engine 503 E-gear box No carbon yet. Compression still 120 per cylinder - like new "outa of the box" Still checking with the dental mirrors and intake and exhaust manifolds off (flashlight down the plug holes) every 50 or so hours. Gotta repaint my muffler once in a while anyway - wish I'd got it chromed when it was new.. Just a test guys - so don't flame me. Don't try this at home - we do this for a living (myth busters - ha ha - I guess I'm Buster). I'm at the Ferguson Farm & I'm the test pilot for "this one" anyway. Never had the jugs off never had the engine even hick up. And I know that's not what the book says. But somebody has to do it. ( Where no man has gone before - 1,000 hr on a 503 CDI no decarb no rebuild Wallmart dot 3 oil "BTW - don't use their aircooled oil") We who are about to die - salute you. (Again -not trying to be disrespectful - we've had our share of fatalities over here - as I'm sure some of you know - but we still fly) http://www.mindspring.com/~possums/ ________________________________________________________________________________
From: "Ralph" <ul15rhb(at)juno.com>
Date: Dec 02, 2005
Subject: Re: 503 de-carbon
Guys, I'm at 450 hours without a teardown or decarbon (2nd engine). I'm running synthetic oil 50:1. Ralph Original Firestar 19 years flying it, Rotax 447 -- possums wrote: At 07:33 PM 11/28/2005, you wrote: > >John, I am at 260 hours with no de-carbon jobs yet. At 150 hours I took it >to a mechanic for service and he said there was no need to tear into it. At >300, I plan to overhaul it and I'm curious to see how it looks inside. Me too - got 669 hours now without a decarb - really. 1999 Engine 503 E-gear box No carbon yet. Compression still 120 per cylinder - like new "outa of the box" Still checking with the dental mirrors and intake and exhaust manifolds off (flashlight down the plug holes) every 50 or so hours. Gotta repaint my muffler once in a while anyway - wish I'd got it chromed when it was new.. Just a test guys - so don't flame me. Don't try this at home - we do this for a living (myth busters - ha ha - I guess I'm Buster). I'm at the Ferguson Farm & I'm the test pilot for "this one" anyway. Never had the jugs off never had the engine even hick up. And I know that's not what the book says. But somebody has to do it. ( Where no man has gone before - 1,000 hr on a 503 CDI no decarb no rebuild Wallmart dot 3 oil "BTW - don't use their aircooled oil") We who are about to die - salute you. (Again -not trying to be disrespectful - we've had our share of fatalities over here - as I'm sure some of you know - but we still fly) http://www.mindspring.com/~possums/ ________________________________________________________________________________
Date: Dec 02, 2005
From: possums <possums(at)mindspring.com>
Subject: Re: 503 de-carbon
At 11:26 PM 12/1/2005, you wrote: > >Guys, > >I'm at 450 hours without a teardown or decarbon (2nd engine). I'm >running synthetic oil 50:1. > >Ralph >Original Firestar >19 years flying it, Rotax 447 Don't go with me - I'M NOT AN ENGINE PERSON I'm just the test dummy. Now "Tom" knows all about your 447. --------- From: "Tom Olenik" <olenik-aviation(at)buyitsellitfixit.com> Subject: <http://www.matronics.com/searching//searching/getmsg_script.cgi?INDEX=35477735?KEYS=possums?LISTNAME=Kolb?HITNUMBER=259?SERIAL=23491830991X?SHOWBUTTONS=NO>Need guidance Rotax 447 I'd like to show a picture of a piston that was making 110 pounds of compression on a 447. The top ring is gone along with most of the piston on the exhaust side above the lower ring. The other piston which was undamaged was at 115 but both pistons were over .008" clearances and all the rings were over .030" end gap. This engine never quit and was running right up to the time when he traded it in on a new 447. Someone had picked up a couple of 447 pistons from a snowmobile shop which followed the cross references to a piston that is actually smaller than the current standard sized. Since no one probably actually measure the clearance, they started out beyond the maximum clearance most likely. At one point Rotax changed the standard sized piston on the 447 to one that is a little larger. This engine came with that larger standard size, but someone installed the smaller standard sized piston. Still ran and still had compression. A compression test on a Rotax engine has very little value. It will tell you if there is a hole in the piston or if there is a differential, it might tell you something, but there is NO specification to go by what it acceptable and what is not. However, you can physically check for stuck rings through the exhaust port. Tom Olenik Olenik Aviation ------------------------ I agree with Tom on most of the points he mentions. However, the 503 is a different animal. It is a rock, it is a stone, it is the pinnacle of the two stroke dual carb 52 HP engines at 85+ pounds. However, I don't agree that a compression test "has very little value" after 8 test over 600 hours' with very little difference. A broken ring "our ultimate nightmare" - would show up. I think a "Stuck ring" would show up even if you neglected to check that with your fingers or a prob. I've flown a 447 with points - on a KXP for at least 400 hours before this one - they are finicky little engines, they want everything to be just right. But...when everything is right, they are hard to beat - you know what I mean. ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: 503 de-carbon
Date: Dec 02, 2005
possums and Group, It is possible that there is no real difference between my engine and those that are running high hours without de-carbon. I may just be too fussy about my oil rings being totally free. I don't check compression and I have not been able to detect a stuck ring through the exhaust port. Also, I have read that the oil rings are not all that important. Maybe, in the future, I will check compression and the exhaust port visual check, and keep flying. John Jung Firestar II N6163J Surprise, AZ On Dec 2, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > Me too - got 669 hours now without a decarb - really. 1999 Engine 503 > E-gear box > No carbon yet. Compression still 120 per cylinder - like new "outa > of the box" Still checking with the dental mirrors and intake and > exhaust manifolds off (flashlight down the plug holes) every 50 or so > hours. ________________________________________________________________________________
From: "Denny Rowe" <rowedl(at)highstream.net>
Subject: Re: Hauling Kolbs on flat beds
Date: Dec 02, 2005
> > Thanx Denny, I've been considering the "wing removed" option too... I > noticed the tail lock in some of the pictures on the net... How long do > the > pieces of pipe need to be?... Unfortunately, I don't have a Kolb locally > to > look at, so I'm going to have to prepare everything before I go to pick it > up... > > Thanx again... > > David > > David My pipes are about 27 inches long 1/2" CPVC with pipe insulation over em, the Tees and Elbows (4 of each) only have about 1/8" inch between each (so you need to cut six short stubs of pipe) and the whole gizmo slides down over the folded tail till it hits the tail cable tangs. As wind will work on it on an open trailer, you want to secure it from sliding up and off with bungee cords or better yet, wrap the entire tail with your plastic wrap. also you want to wrap the lexan windscreen also. Make sure to use primer and the correct cement so there will be no chance of the tail lock comming apart. I like this design a little better than the one in the plans that uses nylon sash cord instead of the Tees and Elbows. Of coarse either work fine. Denny Rowe ________________________________________________________________________________
Date: Dec 02, 2005
From: Jon LaVasseur <firestar503(at)yahoo.com>
Subject: Re: Written test
Hi Ralph, I just talked with Hummingbird Aviation and we will need two forms of ID (drivers license and creidt), your EAA certificate and payment which can be credit/debit, cash or check. They are located near the corner of 212 and Pioneer Trail. __________________________________ ________________________________________________________________________________
Date: Dec 02, 2005
From: Jon LaVasseur <firestar503(at)yahoo.com>
Subject: Re: Written test
Hi Ralph, I just talked with Hummingbird Aviation and we will need two forms of ID (drivers license and creidt), your EAA certificate and payment which can be credit/debit, cash or check. They are located near the corner of 212 and Pioneer Trail. Just $16.99/mo. or less. dsl.yahoo.com ________________________________________________________________________________
Date: Dec 02, 2005
From: Jon LaVasseur <firestar503(at)yahoo.com>
Subject: Re: Written test
Hi Ralph, I just talked with Hummingbird Aviation and we will need two forms of ID (drivers license and creidt), your EAA certificate and payment which can be credit/debit, cash or check. They are located near the corner of 212 and Pioneer Trail. Just $16.99/mo. or less. dsl.yahoo.com ________________________________________________________________________________
Date: Dec 02, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Hauling Kolbs on flat beds
Thanx Denny, any chance of a picture(s)?... I can't get over the excellent advice I've received on this list... I have received several messages off list as well as the on list messages... I'm really excited about picking up my first Kolb in a couple of weeks, but scared to death that I'll damage it hauling it home... And then there's the sanity issue regarding bringing it home on the snow/ice roads... My wife keeps reminding me... Thanx again... David On 12/2/05, Denny Rowe wrote: > > > > > > Thanx Denny, I've been considering the "wing removed" option too... I > > noticed the tail lock in some of the pictures on the net... How long do > > the > > pieces of pipe need to be?... Unfortunately, I don't have a Kolb > locally > > to > > look at, so I'm going to have to prepare everything before I go to pick > it > > up... > > > > Thanx again... > > > > David > > > > David > My pipes are about 27 inches long 1/2" CPVC with pipe insulation over em, > the Tees and Elbows (4 of each) only have about 1/8" inch between each (so > you need to cut six short stubs of pipe) and the whole gizmo slides down > over the folded tail till it hits the tail cable tangs. As wind will work > on > it on an open trailer, you want to secure it from sliding up and off with > bungee cords or better yet, wrap the entire tail with your plastic wrap. > also you want to wrap the lexan windscreen also. > Make sure to use primer and the correct cement so there will be no chance > of > the tail lock comming apart. > I like this design a little better than the one in the plans that uses > nylon > sash cord instead of the Tees and Elbows. Of coarse either work fine. > > Denny Rowe > ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: Wire wheel?
Date: Dec 02, 2005
Is a BRASS wire wheel acceptable for removing old flaky primer and surface rust from 4130 aircraft tubing? Enquiring minds want to know... Jeremy Casey Kilocharlie Drafting, Inc. www.kilocharlie.us ________________________________________________________________________________
From: "Paul Petty" <Lynnp@c-gate.net>
Subject: Ms. Dixie update
Date: Dec 02, 2005
required 4.6, HTML_MESSAGE 0.25) Kolbers, Well it's been 27 months into the construction of Ms. Dixie and I am happy to report that today I reached a major milestone. I had the pleasure of dealing with the fine folks at Grand Rapids. Takes forever to get Sandy on the phone but now I know why. What a pleasant and knowledgeable person to deal with. Between her and Dick at Kuntzlman I am all set to receive the hot box (custom made) and EIS for the Kolbra. Note to any 912 user purchasing a hot box from anywhere... do not pay the $215.00 price because you will receive a $25.00 voltage regulator you cant use. Tell who ever you order it from you have a 912 and if you are going to use a EIS tell them that as well. they custom make the battery cables and leads to the engine. I recommend going straight to the companies them selves. Great people. The reason this is a milestone for me is because this is the last leg of building before disassembly for covering and painting. I want to have a complete running airplane full of fuel,coolant and oil and instruments before I even think of covering. This way if anything needs to be changed or modified or heaven forbid "Leaks" I wont have a problem cleaning up. Thanks to the many that have helped Travis, Mark German, John Hauck just to name a few and with any luck Ms Dixie just may fly this spring or early summer. On another note John Hauck dropped in here yesterday and when I say dropped I mean Dropped. He uses less runway than anyone that lands here...except for maybe Jim Williamson. Like to get those two guys here for a short field competition someday. Well time to head to the shop and clock in take care guys and fly safe! Paul Petty Building Ms. Dixie Kolbra/912UL/Warp ps. 2 new items I found this week for our airplanes. 1. Areoquip fuel line FC332 and 2. Powergrip hose clamps.. e-mail me if you want details and prices. I stock both.:-) ________________________________________________________________________________
From: "Jim Baker" <jlbaker(at)telepath.com>
Date: Dec 02, 2005
Subject: Re: Wire wheel?
> >Is a BRASS wire wheel acceptable for removing old flaky primer and > >surface rust from 4130 aircraft tubing? > > > >Enquiring minds want to know... Got something better for ya...do a search for 3M surface conditioning discs.....come in several different grades and there are other 3M Roloc items that are very nice to work with when cleaning/prepping surfaces..... http://search.store.yahoo.com/cgi- bin/nsearch?query=roloc&first=20&only=0&categ=all&catalog=levine auto or if you don't want to cut/paste... http://tinyurl.com/9jl5v Jim Baker 580.788.2779 '71 SV, 492TC Elmore City, OK ________________________________________________________________________________
Date: Dec 02, 2005
From: ray anderson <rsanoa(at)yahoo.com>
Subject: Re: Firefly forced to Land
Maybe I'm missing something but it seems to me that any pilot in a private plane not up to date and current as to the situation at Camp David on any given day, would have the common sense to assume the the safe thing to do is use always the six mile figure. For heavens sake, why set your self up for a big hassle and embarrassment for a measly three miles horizontally. Anyone that haphazard and careless maybe shouldn't be flying. It's not that I'm so worried about the president, but that kind of stupidity could run all over me somewhere. O.K so I'm in a bad mood, but those kind of things tee me off because it makes things harder for all of us in the long run. "Jack B. Hart" wrote: > < Most of the time, the restricted airspace around Camp David is 12,500 feet high with a radius of three nautical miles, or about 31/2 miles. But when the president is at Camp David, as he was Sunday, the space expands to an altitude of 18,000 feet with a radius of five nautical miles, or nearly six miles. > --------------------------------- Single? There's someone we'd like you to meet. ________________________________________________________________________________
From: "Rick Pearce" <rap(at)isp.com>
Subject: posting on matronics.
Date: Dec 02, 2005
Can I use the photoshare to post the wiring diaram that I was trying to attach the other day?It will be in auto cad. ________________________________________________________________________________
From: "Guy Morgan" <morganguy(at)hotmail.com>
Subject: Wire wheel?
Date: Dec 03, 2005
Jeremy, Check FAA pub AC 43.13 for acceptable practices. It is available online, although I don't have the address at this time. You can download the whole pub in .pdf format. A brass wheel would work provided you go easy with it and don't dwell on one spot for too long at a time. The preferred method is always the least destructive first. I prefer chemical stripping if possible, then plastic media bead blasting, and abrasive last. Hope this helps. Guy Morgan Galveston, TX Firefly From: "Jeremy Casey" <n79rt(at)kilocharlie.us> Subject: Kolb-List: Wire wheel? Date: Fri, 2 Dec 2005 15:27:21 -0500 Is a BRASS wire wheel acceptable for removing old flaky primer and surface rust from 4130 aircraft tubing? Enquiring minds want to know... Jeremy Casey Kilocharlie Drafting, Inc. www.kilocharlie.us ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: airport alternatives
Date: Dec 03, 2005
If I remember right, I think John's main problem with the cows is their "residue" painting the underside of his wings. :-) "Dumber than horses ??" Yah, but that ain't saying much. lol Do not Archive. Lar. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "russ kinne" <kinnepix(at)earthlink.net> Subject: Re: Kolb-List: airport alternatives > > we used to fly from a regular, certificated grass airport where a white > horse shared the runway with us. > Field was 2000' long and plenty wide. When he was on one side, we'd > land (Cessnas, Pipers, the skydiver's jump-plane) on the other. He'd > watch us but never ran around or caused any trouble. Good horse! > I hope John H hasn't had any trouble with cows; they're dumber than > horses by a long shot. ________________________________________________________________________________
Date: Dec 03, 2005
From: bryan green <lgreen1(at)sc.rr.com>
Subject: Re: Firefly forced to Land
Billie I agree with what you have said. One thing that I suggest is that everyone think twice before they bring outsiders like the insurance co. into our business. Kinda like the old glass house thing ya know. It very easy to point out bad things if your not the one thats doing them and consider yourself some what above others. I fly both ultralights and GA and can point out problems with both two examples of this would be. 1. While attending a flyin this year I was presented with the problem of an ultralight playing in the pattern while I was on down wind for landing (flying c-172) had to cut down wind short on short field to keep from running over the guy. 2. While hosting our flyin this year most of the GA pilots flying in made a left hand pattern to 23 and a nice landing. The problem with that was 23 is a right hand pattern denoted with a segmented circle at the field and also listed in the airport and facilities directory. I think the main problem rest with the person that trained these pilots and second with the people that run around blabbing about how stupid ultralight or GA pilots are. I think the best thing to do would be to remember we are all pilots and we all make mistakes. Perhaps it would be better to grow a set and walk up to the person and nicely say I am concerned with your safety while this happened it possibly would be better to do it this way so that we all can fly safely. Like an old chief told me one time it's better if we take care of our own.FWIW Bryan Green Elgin SC bill_joe wrote: > We can all get along if everyone follows and understands the rules. > I hope this helps some of the new ultralite pilots understand the >importance of this. > Thanks, gang. > > > >> >> > > > > ________________________________________________________________________________
Date: Dec 04, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Dimensions...
Latest on Firestar haul... I picked up the trailer yesterday and the bed is 16' X 6' with a 12" rail around the front and sides... Because I don't have a local Kolb to look at, I have been "guesstimating" distances... I need the distance from the main gear to the tailwheel, the distance from outside of main tire to outside of the other and if possible, the distance from the main gear to the tip of the nose... Sorry to be such a "pest", I really appreciate all the help I've received on the List, hopefully, I'll be able to help someone here in the future... Thanx... David ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop noise
Date: Dec 04, 2005
Group, Yesterday, I flew for the first time after raising the engine up a full inch, leaving a 2 inch gap between the prop tip and the boom tube. It was noticeably quieter, than with only 1 inch of clearance. John Jung Firestar II N6163J Surprise, AZ ________________________________________________________________________________
From: "Judy or Larry Gitt" <gittj(at)earthlink.net>
Subject: Hanger
Date: Dec 04, 2005
The way they get around this is to say , we will add your name to the list of 27 that are on the waiting list for a hanger , guess What? It will take years of waiting to get a hanger. The FBO,s they don't want A/C they can't annual or sale gas too . Your home built or Experimental or U/L is not going to pay the bill for them , and im sure if we were in the FBO shoes we would feel the same .There is a big need for hangers in my area but the city just won't spend the money . What we need is a A/C that we can drive it home and park it in our garage, drive it to the Airport and take off . it would put Aviation in a new era. If you had 10 or 50 new pilots in your area where are they going to put there planes ??? You sure don't want to leave them out side . Not with the storms we have been having all across the country. Trailer is fine but you need two people and it is a pain and some times hard to find that other person to help out . Aviation needs to make a nother step forward, in a new designe . Kolb is a great little plane i really enjoy mine but it sure would be nice to drive it home ,not paying hanger rent and work on it when i had time at home . For what it's worth! { Dreamer } Larry ________________________________________________________________________________
From: "Vic" <vicw(at)vcn.com>
Subject: Re: Kolb-List Digest: 22 Msgs - 12/03/05
Date: Dec 04, 2005
Kirk: You are never safe from a law suit. The solution is to have someone defend. If you rent to someone make sure they have insurance and name you as an additional insured. That way, when you get sued (I didn't say "if") you have an attorney to defend you. ________________________________________________________________________________
From: "Michael Bigelow" <orcabonita(at)hotmail.com>
Subject: Prop Clearance
Date: Dec 04, 2005
Im very suprised how many people are running just one inch of prop clearance on thier Kolbs. The increased noise is bad enough, but even worse is you also have a greatly increased chance of a prop strike on the tail boom :( The engines are mounted in rubber mounts which flex, and metal and aluminum also flex given enough force... With a hard landing, or getting into aircraft wake or severe turbulance ( it happens ) could easily reduce that one inch to a negative number ! The top of the tail boom where it connects to the fuselage is the worst place on the entire boom to take any damage as the tensional forces there are greater there than anywhere else on the boom. When you take the center of thrust on the Kolb and compare it to the center of gravity and drag, another inch or two is just not that big a precentage change and should not make much of a difference in the flying qualities. I would not build my MK III with less than 3 inches clearance, and 6 would be better... Im suprised we are not hearing about more boom strikes here. Michael Bigelow Archive ________________________________________________________________________________
From: "Kirk Smith" <snuffy(at)usol.com>
Subject: Re: Kolb-List Digest: 22 Msgs - 12/03/05
Date: Dec 04, 2005
> Kirk: You are never safe from a law suit. The solution is to have someone > defend. If you rent to someone make sure they have insurance and name you > as an additional insured. That way, when you get sued (I didn't say "if") > you have an attorney to defend you. I know.....That was the point I had intended. My solution is to just not rent space on my strip. When you start taking money the rules change significantly. ________________________________________________________________________________
Date: Dec 04, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Re: Dimensions...
Thanx for the pictures Mike... I plan to support the boom, I was just trying to figure out how far it is to the tailwheel so that I could plan the support location... Thanx again... David On 12/4/05, Mike Pierzina wrote: > > > >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> > I need the distance from the main gear to the tailwheel, > > Thanx... > > David > <>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> > > David, > Why do you need the tailwheel distance....hasn't anyone told you to > support your plane by making a "saddle" for > The boom tube......usually in front of the empanage , so that you can > "strap" it to the tube.....The tailwheel shouldn't touch during > transport..... > > Here's some pictures of my 21' plane on my 10' trailer ( it's in the > Matronics "photo share" ) > > > http://www.matronics.com/photoshare/planecrazzzy@yahoo.com.05.02.2005/ > > ________________________________________________________________________________
Date: Dec 04, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: on't Want to Become a Sport Pilot"
From December 2005, Sport Pilot, Page 72. "You might want to get rid of some of the gauges, too. All you really need is a yaw string; you can feel the wind in your face and see the ground. You're an ultralight pilot; you should be one with your vehicle...Zen... enjoying seat-of-pants, grassroots flying." I believe this is terrible advice. One of the quickest ways to put FAR Part 103 at risk is to increase the kill rate for grassroots 103 pilots. Wind in your face and seeing the ground is not adequate in that many will believe what they see over what they feel. The end result is a stall and nose into the ground when turning from down wind to base. The opposite condition leads to departure stalls. If instruments are available, observed and believed, both of these conditions are preventable. One can keep a radio and gps off the vehicle by wearing it, but it is difficult to do the same for airspeed, altitude, and rate of climb indicators, and cylinder head and exhaust gas temperature indicators. To fly without any of these puts the 103 pilot at greater risk. Jack B. Hart FF004 Winchester, IN EAA 45676 ________________________________________________________________________________
From: "Vince Nicely" <vincenic(at)xtn.net>
Subject: Re: Hanger - Trailering Works
Date: Dec 04, 2005
Larry and Others, I changed the title line slightly. My experience with trailering is good and it requires only one person. >The statement made was: Trailer is fine but you need two people and it >is a pain and some times hard to find that other person to help out . >Aviation needs to >make another step forward, in a new designe . Kolb is >a great little plane i really enjoy mine but it sure would be nice to drive >it home ,not paying hanger rent >and work on it when i had time at home . >For what it's worth! Sorry, in my experience, the Kolb is very trailerable and does not need a second person to assist in assembly or disassembly. I have been tailering my Kolb to/from the airport every time I fly it over the last 10 years and presently have 380 hours on it. In addition to my Firestar II, I made a simple and open trailer with a tilt bed along with a simple tripod to support a wing tip. I can easily roll the folded Kolb on/off the trailer by hand and with no help. When I wish to unfold the Kolb, I have a tripod that I sit near where the wing tip will be. I open the wing and sit its outside end on the tripod. The inner, front tip is supported on the bow for the full enclosure I use. If you do not have a full enclosure, adding a temporary support for the front edge would be relatively easy. With the wing supported, I have my hands free to walk around and to insert the pins needed to make the Kolb flyable. Very simple, and it only takes a few minutes. Because I usually fly 2 to 3 hours when I go out, I estimate I have done the fold/unfold approximately 150 times with no problems. I keep my folded Kolb in one side of my garage and use it when I have time. I just wanted all those who might want to store and trailer their Kolb to know that with a simple jig or two, it is easily done by one person and provides a very nice way to have an airplane without a hanger. Vince Nicely ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: RE:
Date: Dec 04, 2005
Pardon my jumping in, but I have to respectfully disagree. In fact, I think that if you can't fly a light aircraft or ultralight without the aid of gauges, you probably shouldn't be solo. At least, you should still be under an instructors supervision until such time as you can fly seat-of-the-pants. An overreliance on the appearance of the ground, to the point that a stall occurs in a downwind turn or similar situation is a training issue, IMO. Treating that with instrumentation is the wrong fix. Good seat-of-the-pants flying skills are vital particularly for the light aircraft pilot. Gauges and instruments are fallible and give false information or fail at the worst possible times. But good stick-rudder/control bar (if you're a triker) skills never malfunction and always give the correct responses to the pilot. This is even true in most general aviation a/c - extensive reliance on instruments for flight generally only starts once you get into larger complex aircraft. But any ultralight should be flyable completely without any instrumentation whatsoever. Generally, an ASI is a good idea in a 3-axis plane at first (not needed in a trike however), but generally you should be able to fly without one within 25 to 50 hours or thereabouts. I submit this should even be practiced on a frequent basis once you get some hours under your belt in the plane. Personally, if I were allowed one and only one flight instrument in my airplane it'd be an altimeter. Altitude is the hardest to judge without a gauge. The rest should only be nice to have in a light aircraft, and _never_ essential for flight.... JMHO, LS N646F . >Subject: "Don't Want to Become a Sport Pilot" > > >From December 2005, Sport Pilot, Page 72. > >"You might want to get rid of some of the gauges, too. All you really need >is a yaw string; you can feel the wind in your face and see the ground. >You're an ultralight pilot; you should be one with your vehicle...Zen... >enjoying seat-of-pants, grassroots flying." > >I believe this is terrible advice. One of the quickest ways to put FAR >Part >103 at risk is to increase the kill rate for grassroots 103 pilots. Wind >in >your face and seeing the ground is not adequate in that many will believe >what they see over what they feel. The end result is a stall and nose into >the ground when turning from down wind to base. The opposite condition >leads to departure stalls. If instruments are available, observed and >believed, both of these conditions are preventable. > >One can keep a radio and gps off the vehicle by wearing it, but it is >difficult to do the same for airspeed, altitude, and rate of climb >indicators, and cylinder head and exhaust gas temperature indicators. To >fly >without any of these puts the 103 pilot at greater risk. > >Jack B. Hart FF004 >Winchester, IN >EAA 45676 > > ________________________________________________________________________________
Date: Dec 04, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Re: Hanger - Trailering Works
Vince is not exaggerating. Many times I have watched him unload and set up his Firestar by himself. Or fold it up and put it back on the trailer. In fact, when I offer to help, I am told to stay out of the way, he can do it quicker by himself. And it really does happen pretty quick, I would say 15-20 minutes from the time he gets out of the car until the airplane is assembled, the preflight is done and he is ready to start the engine. Compared to spending a grand or two a year for hangar rent, it's not unreasonable. And what you saved on hangar rent will buy you a new Rotax every third year... Richard Pike MKIII N420P (420ldPoops) > > >Sorry, in my experience, the Kolb is very trailerable and does not need a >second person to assist in assembly or disassembly. I have been tailering >my Kolb to/from the airport every time I fly it over the last 10 years and >presently have 380 hours on it. In addition to my Firestar II, I made a >simple and open trailer with a tilt bed along with a simple tripod to >support a wing tip. > >I can easily roll the folded Kolb on/off the trailer by hand and with no >help. When I wish to unfold the Kolb, I have a tripod that I sit near where >the wing tip will be. I open the wing and sit its outside end on the >tripod. The inner, front tip is supported on the bow for the full enclosure >I use. If you do not have a full enclosure, adding a temporary support for >the front edge would be relatively easy. With the wing supported, I have >my hands free to walk around and to insert the pins needed to make the Kolb >flyable. Very simple, and it only takes a few minutes. Because I usually >fly 2 to 3 hours when I go out, I estimate I have done the fold/unfold >approximately 150 times with no problems. > >I keep my folded Kolb in one side of my garage and use it when I have time. >I just wanted all those who might want to store and trailer their Kolb to >know that with a simple jig or two, it is easily done by one person and >provides a very nice way to have an airplane without a hanger. > >Vince Nicely > > ________________________________________________________________________________
Date: Dec 04, 2005
From: Earl & Mim Zimmerman <emzi(at)supernet.com>
Subject: Re: RE: Seat-of-the-Pants
Well said Lucien!! ~ Earl lucien stavenhagen wrote: > > Pardon my jumping in, but I have to respectfully disagree. > In fact, I think that if you can't fly a light aircraft or ultralight > without the aid of gauges, you probably shouldn't be solo. At least, you > should still be under an instructors supervision until such time as you can > fly seat-of-the-pants.--------------------- -- ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: Hanger
Date: Dec 04, 2005
I think it depends a lot on your situation. I agree with you, and with Ray, Vince and Richard. Squeezing Vamoose into that tiny trailer of mine works, but it's an exercise in strain and frustration.........and the thing hasn't even flown yet. Arizona Dave has his down to a science and zips his Mk III right in there, tho' his trailer is a *little* larger. I haven't seen this for myself, but my thought is that Jim Hefner has the right idea. His trailer is huge, and that little FireFly must be a breeze to load and unload. (wanna swap trailers, Jim ??) :-) I thought I was saving a few bucks on the trailer I bought for Vamoose - and I did - but it was false economy. Wish now that I'd waited, spent more money, (if necessary) and gotten a bigger trailer. Wiser Lar. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "Judy or Larry Gitt" <gittj(at)earthlink.net> Subject: Kolb-List: Hanger > > > The way they get around this is to say , we will add your name to the > list of 27 that are on the waiting list for a hanger , guess What? It will > take years of waiting to get a hanger. The FBO,s they don't want A/C > they can't annual or sale gas too . Your home built or Experimental or > U/L is not going to pay the bill for them , and im sure if we were in > the FBO shoes we would feel the same .There is a big need for hangers in > my area but the city just won't spend the money . What we need is a A/C > that we can drive it home and park it in our garage, drive it to the > Airport and take off . it would put Aviation in a new era. If you had 10 > or 50 new pilots in your area where are they going to put there planes > ??? You sure don't want to leave them out side . Not with the storms we > have been having all across the country. Trailer is fine but you need > two people and it is a pain and some times hard to find that other person > to help out . Aviation needs to make a > nother step forward, in a new designe . Kolb is a great little plane i > really enjoy mine but it sure would be nice to drive it home ,not paying > hanger rent and work on it when i had time at home . For what it's worth! > { Dreamer } Larry > > > ________________________________________________________________________________
From: russ kinne <kinnepix(at)earthlink.net>
Subject: q
Date: Dec 04, 2005
List I apologise -- thought I was emailing Jim B directly, but it went onto the list -- without the DNA tag. Sorry. ________________________________________________________________________________
From: "Kolbdriver" <Kolbdriver(at)bellsouth.net>
Subject: Re: Hanger
Date: Dec 04, 2005
Trailer is fine but you need two people and it is a pain and some times hard to find that other person to help out . Larry, I have kept my MK III in a trailer and at home for the 5 years I've had it flying. It takes 20 minutes to unload and assemble or 20 minutes to fold, load and tie down, all done solo. This past summer I mowed a landing strip behind the house and plan to build a hanger/shed in the future. I have had hanger space offered but prefered to spend that money on something else. Steven Green N58SG MK III 912S 400 hrs ________________________________________________________________________________
Date: Dec 04, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Re: RE: Seat-of-the-Pants
Lucien, Earl, and Kolbers, I agree with you! I did not intend to imply overuse or the need for instruments while flying a 103 vehicle. Good stick and rudder habits should be a given, but why give up instruments that can help you analyze unusual situations? Why do so many 103 pilots roll their vehicles into a ball below the pattern? Is it lack of good stick and rudder training and/or inability to react properly to what instruments indicate? I believe it may be a combination of both plus some pilot distraction. I like my vertical air speed indicator the best. It lets me detect ridge rotors, and high speed thermal sink early, and on very very hot days tells me if I can maintain a healthy climb rate The slip indicator could be removed. It is nice to have because once the FireFly was trimmed out at zero degree flaperons and at cruise, one can adjust the flaperons and reduce drag at off cruise speeds while maintaining constant altitude. Once you move off normal cruise speed, P-factor comes back into play and the FireFly starts slipping. At above normal cruise speeds, one can pick up a little more speed by re flexing the flaperons a bit. Not important for bumming around, but it helps stretch five gallons of fuel on cross countries. Altimeter and air speed indicator could be replaced with the gps and throttle position as an in flight speed reference. Typically I like to fly 2,000 to 3,000 feet above ground level so that if the engine quits, I have a few minutes to pick a landing spot within a two to three mile radius. As long as I have to run a two cycle engine, I would find it difficult to give up engine instruments. If used properly, I believe instruments expand the pilots ability to fly in a safer and more efficient manner that with out them. And because others are flying in and around my home and neighboring airports, I like to use a gps and radio too. But what instruments to use is a personal choice that every 103 pilot must make. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
From: "Richard & Martha Neilsen" <NeilsenRM05(at)comcast.net>
Subject: Re: Prop Clearance
Date: Dec 04, 2005
Mike/All I agree that 1 inch is a bit close but I had 7 inches of clearance on my 72 inch prop and that was way too much of a high thrust line. Full power with a high thrust line is not fun. If you are at the lower end of your speed range like you are in take off, climb or needing to make a go around on a short strip it can bite you. When you are at the forward end of your weight and balance (like when you have a passenger) it gets worse. I have been there and I spent allot of time and effort to LOWER my thrust line. Don't get carried away with it two inches of clearance is plenty. Rick Neilsen Redrive VW powered MKIIIc ----- Original Message ----- From: "Michael Bigelow" <orcabonita(at)hotmail.com> Subject: Kolb-List: Prop Clearance > > > Im very suprised how many people are running just one inch of prop > clearance > on thier Kolbs. The increased noise is bad enough, but even worse is you > also have a greatly increased chance of a prop strike on the tail boom :( > The engines are mounted in rubber mounts which flex, and metal and > aluminum > also flex given enough force... With a hard landing, or getting into > aircraft wake or severe turbulance ( it happens ) could easily reduce that > one inch to a negative number ! The top of the tail boom where it > connects > to the fuselage is the worst place on the entire boom to take any damage > as > the tensional forces there are greater there than anywhere else on the > boom. > > When you take the center of thrust on the Kolb and compare it to the > center > of gravity and drag, another inch or two is just not that big a precentage > change and should not make much of a difference in the flying qualities. > I > would not build my MK III with less than 3 inches clearance, and 6 would > be > better... Im suprised we are not hearing about more boom strikes here. ________________________________________________________________________________
From: "Ed Chmielewski" <edchmiel(at)mindspring.com>
Subject: Re: RE: Seat-of-the-Pants
Date: Dec 05, 2005
Kolbers All, I must be crazy but I consider an airspeed indicator an essential device, up there with CHT/EGT or RPM gauge. My ears (and butt) just aren't that finely tuned to sense decaying airspeed due to wind shear or shift, and that's when one needs it most. It's a must-have for me. I'm not saying one can't fly the plane without it (pitch + power = performance and all that), but it makes it much easier and can save one's bacon on occasion. Not picking on ya Jack, but some things stuck out: > I agree with you! I did not intend to imply overuse or the need for > instruments while flying a 103 vehicle. I don't think an ASI can be overused. One can always ignore it. > Good stick and rudder habits should be a given, but why give up > instruments > that can help you analyze unusual situations? Why do so many 103 pilots > roll their vehicles into a ball below the pattern? Precisely. Probably because they were ignoring the ASI for starters. An ASI doesn't prevent stall/spin accidents, but it can help avoid them much more than one's tush IMO. > I like my vertical air speed indicator the best. It lets me detect ridge > rotors, and high speed thermal sink early, and on very very hot days tells > me if I can maintain a healthy climb rate ? I think it's VSI. (grin) I agree the VSI helps on those occasions and others. At above normal cruise > speeds, one can pick up a little more speed by re flexing the flaperons a > bit. Not important for bumming around, but it helps stretch five gallons > of fuel on cross countries. How do you know you're changing a few knots without an ASI? > Altimeter and air speed indicator could be replaced with the gps and > throttle position as an in flight speed reference. Typically I like to > fly > 2,000 to 3,000 feet above ground level I suppose one could put notches, magic marker or tape next to the throttle lever to indicate RPM. And hope a plug doesn't foul, or a cable don't stretch, or an air leak develop... Seriously, GPS lags much more than an ASI, and I've seen it be quite inaccurate on some days. The GPS's I've used don't tell AGL, but MSL when given the local altimeter. The GPS makes a nice backup, but I wouldn't rely on it for primary info. (Other than where the he!! on the planet I'm precisely at, of course.) ; ) > As long as I have to run a two cycle engine, I would find it difficult to > give up engine instruments. If you're in an airplane, why not have a couple of airplane instruments (ASI/altimeter)? I think the airspeed of my craft is important, and there are times when I am very interested in its smallest change. Just my opinion, folks. Ed in JXN MkII/503 ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop Clearance
Date: Dec 05, 2005
Michael and Group, The reason that I wasn't concerned about a prop strike with one inch of clearance was that the 68" prop on a Firestar was recommended to me by the designer, Dennis S. Also, I didn't have a prop strike in 4 years of running that way. John Jung Firestar II N6163J Surprise, AZ On Dec 5, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > > Im very suprised how many people are running just one inch of prop > clearance > on thier Kolbs. The increased noise is bad enough, but even worse is > you > also have a greatly increased chance of a prop strike on the tail boom > :( > ________________________________________________________________________________
From: "Wayne T. McCullough" <blackbird754(at)alltel.net>
Subject: Re: RE: Seat-of-the-Pants
Date: Dec 05, 2005
And just a quick reply to all , I was taught...........Airspeed and Altitude are a pilots best friends... Wayne McCullough President EAA chapter 330 Kolbra # 004 ----- Original Message ----- From: "Ed Chmielewski" <edchmiel(at)mindspring.com> Subject: Re: Kolb-List: RE: Seat-of-the-Pants > > > Kolbers All, > > I must be crazy but I consider an airspeed indicator an essential > device, up there with CHT/EGT or RPM gauge. My ears (and butt) just > aren't > that finely tuned to sense decaying airspeed due to wind shear or shift, > and > that's when one needs it most. It's a must-have for me. I'm not saying > one > can't fly the plane without it (pitch + power = performance and all that), > but it makes it much easier and can save one's bacon on occasion. > > Not picking on ya Jack, but some things stuck out: > > >> I agree with you! I did not intend to imply overuse or the need for >> instruments while flying a 103 vehicle. > > I don't think an ASI can be overused. One can always ignore it. > >> Good stick and rudder habits should be a given, but why give up >> instruments >> that can help you analyze unusual situations? Why do so many 103 pilots >> roll their vehicles into a ball below the pattern? > > Precisely. Probably because they were ignoring the ASI for starters. An > ASI doesn't prevent stall/spin accidents, but it can help avoid them much > more than one's tush IMO. > >> I like my vertical air speed indicator the best. It lets me detect ridge >> rotors, and high speed thermal sink early, and on very very hot days >> tells >> me if I can maintain a healthy climb rate > > ? I think it's VSI. (grin) I agree the VSI helps on those occasions > and others. > > At above normal cruise >> speeds, one can pick up a little more speed by re flexing the flaperons a >> bit. Not important for bumming around, but it helps stretch five gallons >> of fuel on cross countries. > > How do you know you're changing a few knots without an ASI? > >> Altimeter and air speed indicator could be replaced with the gps and >> throttle position as an in flight speed reference. Typically I like to >> fly >> 2,000 to 3,000 feet above ground level > > I suppose one could put notches, magic marker or tape next to the throttle > lever to indicate RPM. And hope a plug doesn't foul, or a cable don't > stretch, or an air leak develop... Seriously, GPS lags much more than an > ASI, and I've seen it be quite inaccurate on some days. The GPS's I've > used > don't tell AGL, but MSL when given the local altimeter. The GPS makes a > nice backup, but I wouldn't rely on it for primary info. (Other than > where > the he!! on the planet I'm precisely at, of course.) ; > ) > >> As long as I have to run a two cycle engine, I would find it difficult to >> give up engine instruments. > > If you're in an airplane, why not have a couple of airplane instruments > (ASI/altimeter)? > > > I think the airspeed of my craft is important, and there are times > when I am very interested in its smallest change. Just my opinion, folks. > > Ed in JXN > MkII/503 > > > ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: Wire wheel?
Date: Dec 05, 2005
Thanks for the tip...got a couple locally to try out. Jeremy -----Original Message----- From: Jim Baker [mailto:jlbaker(at)telepath.com] Subject: Re: Kolb-List: Wire wheel? > >Is a BRASS wire wheel acceptable for removing old flaky primer and > >surface rust from 4130 aircraft tubing? > > > >Enquiring minds want to know... Got something better for ya...do a search for 3M surface conditioning discs.....come in several different grades and there are other 3M Roloc items that are very nice to work with when cleaning/prepping surfaces..... http://search.store.yahoo.com/cgi- bin/nsearch?query=roloc&first=20&only=0&categ=all&catalog=levine auto or if you don't want to cut/paste... http://tinyurl.com/9jl5v Jim Baker 580.788.2779 '71 SV, 492TC Elmore City, OK ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: Wire wheel?
Date: Dec 05, 2005
Thanks... Jeremy Jeremy, Check FAA pub AC 43.13 for acceptable practices. It is available online, although I don't have the address at this time. You can download the whole pub in .pdf format. A brass wheel would work provided you go easy with it and don't dwell on one spot for too long at a time. The preferred method is always the least destructive first. I prefer chemical stripping if possible, then plastic media bead blasting, and abrasive last. Hope this helps. Guy Morgan Galveston, TX Firefly From: "Jeremy Casey" <n79rt(at)kilocharlie.us> Subject: Kolb-List: Wire wheel? Date: Fri, 2 Dec 2005 15:27:21 -0500 Is a BRASS wire wheel acceptable for removing old flaky primer and surface rust from 4130 aircraft tubing? Enquiring minds want to know... Jeremy Casey Kilocharlie Drafting, Inc. www.kilocharlie.us ________________________________________________________________________________
From: "Judy or Larry Gitt" <gittj(at)earthlink.net>
Subject: Hanger Trailers
Date: Dec 05, 2005
Hay, guys I'm not nocking the trailer and if you can do it your self that great , I had other U/L the wings fold up , and cost me trying to do it by my self , I well take a exter hand from now on . I'm lucky i share a hanger were i don't have that problem . And it always nice to have your own strip and hanger . Kolbra Larry ________________________________________________________________________________
From: "JIM HEFNER" <hefner_jim(at)msn.com>
Subject: Re: Hangar
Date: Dec 05, 2005
Since I use my trailer as my hangar, it is nice having a large trailer.... 27' x 8.5' on the floor inside. The trailer is parked at the airport most of the year, snuggled nose first into the T part of the hangar on the end.... no problem with microbursts parked there! I roll the plane out and 10-12 minutes later I'm taxiing.... I did it in 8 minutes once just to see how fast I could do it. Most of the GA guys take quite a bit longer than that for preflight. The Firefly is light enough that I can easily pull it up the ramps tail first. I pay $12.50 a year to park the trailer at the airport.... my kind of hangar fees!! I even have electric hooked up to the trailer from the adjacent hangar via extension cord.... nice to have lights and power to charge batteries, radio, etc when I stay overnight. My trailer is big enough to hold all my gear, fuel and I can get a cot in there, even with the plane in the trailer. For hauling the plane, it works well but can be a problem on really windy days... I often haul it at night when winds are light. It weighs 2200#, which is pretty light for a trailer of that size. The tandem axles are great for smooth hauling. I've thought about buying or building a smaller lightweight trailer for when I pull the plane on trips, but decided I didn't need one more trailer sitting around most of the time. This one is a good compromise for using as a hangar and for hauling on trips. To get a Mark III in there would require a winch for sure. AZ Dave has a winch for his and it sits really low compared to my trailer. Lots of difference in weight of a Firefly and a Mark III!! Having to use a winch would take a lot longer and would make using the trailer as a hangar a lot more painful! I'm very happy with my setup. I pulled the trailer/plane 1750 miles and flew some incredible places, including Monument Valley, in May. Hope to do more of that in the future! Jim Hefner Tucson, AZ Firefly #022 219 hrs 1" prop clearance on the 66" IVO 2 blade... I think it depends a lot on your situation. I agree with you, and with Ray, Vince and Richard. Squeezing Vamoose into that tiny trailer of mine works, but it's an exercise in strain and frustration.........and the thing hasn't even flown yet. Arizona Dave has his down to a science and zips his Mk III right in there, tho' his trailer is a *little* larger. I haven't seen this for myself, but my thought is that Jim Hefner has the right idea. His trailer is huge, and that little FireFly must be a breeze to load and unload. (wanna swap trailers, Jim ??) :-) I thought I was saving a few bucks on the trailer I bought for Vamoose - and I did - but it was false economy. Wish now that I'd waited, spent more money, (if necessary) and gotten a bigger trailer. Wiser Lar. ________________________________________________________________________________
From: "b young" <by0ung(at)brigham.net>
Subject: kolb airport, safty
Date: Dec 05, 2005
Ultralite are aloud to fly here they will no longer insure the airport. It is a big mess, they are going to have a hearing on the 8th of this month. All ultralites should have at least a handheld radio and follow the rules set be the FAA around airports. --------------------------------------------- remind those in charge that unless it is a controlled airport that the use of a radio is not required.... it is a very good idea but not a requirement..... also you should observe some of the other operations at the airport and document some of the others that do not follow the guidelines..... example... an ex military plane.... t33 jet.... at my field, while others are in the pattern comes on the radio and announces " t33 jet ( cant remember the manufacture or tail number ) is on a 15 mile straight in final, everybody get out of my way" it seems to me that he did not want to burn the extra fuel necessary to go around and join the pattern properly.... some how he seemed to think he owned the place because he burned more gal/hour than the rest of us.... now the odd part is that the city airport director was real happy to have him around because of the uniqueness of the aircraft... also that he could justify the need for a longer runway because of the needs of the faster aircraft.... when this event happened I had just turned final.... and because he would routinely make a high speed pass at 250 ( plus) I just got as far away as possible as I was not wanting a push.... it seems to me that a "ul" is not a safety problem..... it is the level of education and willingness of the pilot to use the education properly that makes an airport safe, not the type of plane flown.... now it seems that many of the ul pilots do not have the level of training as do private pilots.... but the issue should be " if you will get some training so you can join the rest of us safely, you can use the airport, if not you should stay away until you get some training." and this should include t33 jet drivers as well........ if you would like to use any of this during the hearing please feel free to do so. boyd young brigham city utah. do archive ________________________________________________________________________________
From: "JIM HEFNER" <hefner_jim(at)msn.com>
Subject: Re: Seat of the pants
Date: Dec 05, 2005
Ray, I agree with you. I can fly comfortably without any instrument but ASI. I flew once when I forgot to remove the red flag and had no problem landing, but for safety sake I wouldn't make that a habit. I generally land at idle with with full flaps, so I'm flirting around stall speed and wouldn't do that if I didn't have an ASI instrument to look at.... I could land with partial power or no flaps with more speed without it, but I like having the plane done flying when it touches down and it's good practice for engine out landings. The VSI is the 2nd most useful instrument and the altimeter is the least used instrument for the kind of flying I do. Jim Hefner Tucson, AZ Firefly #022 219hrs ________________________________________________________________________________
From: DCulver701(at)aol.com
Date: Dec 05, 2005
Subject: Re: Hangar
Hi Jim, that is a nice write-up on trailer usage! Who is the manufacturer, and how much did it cost? Saw most of the pictures posted on Monument valley, what a gorgeous place. The pictures from the air are fantastic, compared to ground shots. Hopefully i will make it there someday. Best regards, Dave Culver ________________________________________________________________________________
From: "JIM HEFNER" <hefner_jim(at)msn.com>
Subject: Re: Re: Hangar
Date: Dec 05, 2005
Hi Jim, that is a nice write-up on trailer usage! Who is the manufacturer, and how much did it cost? Saw most of the pictures posted on Monument valley, what a gorgeous place. The pictures from the air are fantastic, compared to ground shots. Hopefully i will make it there someday. Best regards, Dave Culver ------------------------------------ Hi Dave, the trailer was custom built. It's built mostly from 1" square steel tubing. The floor is 1/2" plywood to keep the weight down, so it gives a little when you walk on it but it's plenty stong. The original owner said he paid $4500 to have it custom built. He had it around 8-10 years and had just put new tires on it when I bought it from him. I pulled it from Tucson up to Seattle, to Arlington airport, where I purchased the Firefly and hauled it home in it. At that time I was pulling it with a Ford Explorer. Now I have a 5.4L V8 Expedition, which is much better suited for pulling it. It has a side entry door on the right side near the front. Ramps store in racks underneath behind the wheels. Contact me off-list if you want more info, pic's, etc. Jim ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Prop Clearance
Date: Dec 05, 2005
Hi Michael B/Gang: Thought I would respond to your post: | Im very suprised how many people are running just one inch of prop clearance | on thier Kolbs. The increased noise is bad enough, but even worse is you | also have a greatly increased chance of a prop strike on the tail boom :( I have 3/4" clearance between prop tip and tail boom. If there was a chance of of blade strike, I would increase the clearance. | The engines are mounted in rubber mounts which flex, and metal and aluminum | also flex given enough force... With a hard landing, or getting into | aircraft wake or severe turbulance ( it happens ) could easily reduce that | one inch to a negative number ! Don't think so!!! Take a close look at the Lord Mounts we use for engine mounts. Where do you get your info? | When you take the center of thrust on the Kolb and compare it to the center | of gravity and drag, another inch or two is just not that big a precentage | change and should not make much of a difference in the flying qualities. But it does make a lot of difference. | I would not build my MK III with less than 3 inches clearance, and 6 would be | better... Im suprised we are not hearing about more boom strikes here. If there was a problem, we would be hearing of blade strikes on the tail boom. However, I don't personally know of anyone who has experienced this. I think you will be very unhappy with that much clearance. I believe you might find you get much better performance and handling with a minimum prop tip clearance to the boom tube. Probably be a good idea to qualify these types of comments so the new comer will know from whence they come!!! john h MKIII - 2,444.0 hours 912S - 1,098.1 hours Ultrastar, 1984, and a Firestar, 1987 hauck's holler, alabama | ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 05, 2005
| Personally, if I were allowed one and only one flight instrument in my | airplane it'd be an altimeter. Altitude is the hardest to judge without a | gauge. The rest should only be nice to have in a light aircraft, and | _never_ essential for flight.... | | JMHO, | | LS | N646F Hi LS/Gang: Reckon I'll have to disagree with this one too. ;-) Personally, I can see the ground a hell'uva lot easier than I can see stall speed. Stall speed is much more important than knowing how high I am, in my own humble opinion. Even is an air speed indicator is not calibrated accurately, it will always indicate the same stall speed, no matter what altitude. From my poor memory, most Kolb fatal accidents are the result of stalls low to the ground. Folks forget to cross check their airspeed indicators, or they rely on their "instincts" to keep them above stall speed. Very, very difficult to determine accurate airspeed by the seat of the pants, especially when turning down wind at very low altitudes. john h MKIII/912S hauck's holler, alabama ________________________________________________________________________________
Date: Dec 05, 2005
From: Mitty <benny_bee_01(at)yahoo.com>
Subject: You know that you live in 2005 when...
0.22 FROM_HAS_ULINE_NUMS From": contains.an.underline.and.numbers/letters(at)roxy.matronics.com YOU KNOW YOU ARE LIVING IN 2005 when... 1. You accidentally enter your password on the microwave. 2. You haven't played solitaire with real cards in years. 3. You have a list of 15 phone numbers to reach your family of 3. 4. You e-mail the person who works at the desk next to you. 5. Your reason for not staying in touch with friends and family is that they don't have e-mail addresses. 6. You pull up in your own driveway and use your cell phone to see if anyone is home to help you carry in the groceries. 7. Every commercial on television has a web site at the bottom of the screen. 8. Leaving the house without your cell phone, which you didn't have the first 20 or 30 (or 60) years of your life, is now a cause for panic and you turn around to go and get it. 10. You get up in the morning and go on line before getting your coffee. 11. You start tilting your head sideways to smile. : ) 12. You're reading this and nodding and laughing. 13. Even worse, you know exactly to whom you are going to forward this message. 14. You are too busy to notice there was no #9 on this list. 15. You actually scrolled back up to check that there wasn't a #9 on this list. AND NOW U R LAUGHING at yourself. Go on, forward this to your friends you know you want to! Have a good holidays,everyone! http://home.earthlink.net/~mr_d/index.html Just $16.99/mo. or less. dsl.yahoo.com ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: RE: Seat-of-the-Pants/No Instruments???
Date: Dec 05, 2005
| ... Seriously, GPS lags much more than an | ASI, and I've seen it be quite inaccurate on some days. | > As long as I have to run a two cycle engine, I would find it difficult to | > give up engine instruments. | I think the airspeed of my craft is important, and there are times | when I am very interested in its smallest change. Just my opinion, folks. | | Ed in JXN | MkII/503 Hi Ed/Gang: Good post. GPS is fine for informing me of how fast I am moving over the ground, but has nothing to do with air speed. Air speed is important to me to keep me flying. Yep, I can fly an airplane and a helicopter (well, last time I was flying helicopters) with the instrument panel blanked out, but that was part of training, not something to do at all times. I can fly without an engine and engine instruments, Jack H, but I need that air speed indicator to keep me honest, especially when maneuvering near the ground. I agree with Ed 100% on the airspeed indicator being the most important instrument in my Kolb. john h ________________________________________________________________________________
From: "Ed Chmielewski" <edchmiel(at)mindspring.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 05, 2005
Hi John/All, I agree. I agree with the other statements about not 'absolutely' needing an ASI. The airplane doesn't know it's there, and will fly. But the pilot needs it on several occasions, even day VFR, so it's a must-have IMO. It also occurred to me how much different ops (and 'feel') are in higher elevations and higher density altitude. I was amazed the first time I took a Cessna 421 twin into Albuquerque one July day many years ago. I'd slowed down to normal pattern speed of 120 kts, 100 over the fence, yet the visible groundspeed and sight picture told me we were near cruise. Had to really trust the ASI on that one. The simple 'pitch + power' protocol would've had us in the weeds before the threshold. I know it's not a Kolb, but the correlation still works for C-150s, ULs, etc. We routinely crash RC aircraft at my club, usually base-to-final, because we rely only on visual cues. By the time I see a wing drop, it's too late. 'Nother one bites the dust... Ed in JXN MkII/503 ----- Original Message ----- From: "John Hauck" <jhauck(at)elmore.rr.com> Subject: Re: Kolb-List: RE: Flying without instruments??? Very, very difficult to determine accurate airspeed by the > seat of the pants, especially when turning down wind at very low > altitudes. > > john h > MKIII/912S > hauck's holler, alabama ________________________________________________________________________________
From: "Michael Bigelow" <orcabonita(at)hotmail.com>
Subject: Re: Seat of the pants
Date: Dec 05, 2005
You should at minimun have an airspeed indicator to fly safely. We should all have the skill to fly without the ASI it should it fail, but it is NOT something you should make a habbit of doing. Even though many of have the skill to fly without an airspeed indicator, if you do it on a regular basis, sooner or later it will probably catch up with you. We all get distracted, have bad days, etc. etc. and having the ASI can prevent a disastorous situation. We train for lots of difficult situations in flying, and we are expected to be able to be able to handle them, but that does not mean we should be exposing ourselves to unnecessary risk on a regular basis. An ASI is an important instrument, that gives you information critical for safe flight. Like any insturment it can fail, or mislead you, so you dont want to be overly reliant on it.... But that does not change the fact that it is just plain foolish to routinely fly an ultralight without a working ASI. Michael Bigelow ________________________________________________________________________________
From: "Michael Bigelow" <orcabonita(at)hotmail.com>
Subject: Re: Prop Clearance
Date: Dec 05, 2005
The feedback on prop clearance has been very helpful. I dont want the extra noise and am still not confortable with just one inch, but given your reports I will most definately not go more than 2 or 3 inches. You guys helped me avoid a mistake before it was built into my plane, thanks guys !!! Michael Bigelow ________________________________________________________________________________
From: GeoR38(at)aol.com
Date: Dec 06, 2005
Subject: Re: RE: Seat-of-the-Pants/No Instruments???
OK Ray, I retract seat of the pants and substitute "elbow torque". -however, I have been subjected to several minutes of "fill the pants" flying in my lifetime. :) do I detect a CLASSIC statement here? Well, guys I know we are beating a dead horse at this stage but for some reason, I cannot let this thought go unsaid. I feel sorry for the poor lil EGT meter. It gets almost NO credit ...even amongst such heavies as populate this list. And its absence has popped up and bit us many, many times.... and we STILL don't give it proper praise. Its absence on such early models as the Weedhopper and Pterodactyl which used many Cuyuna engines, brought them down to mother earth like flies, on a chilly day. And we said "those damn Cuyunas ought to be boat anchors." I know, I was one of those brought down...at least 3 times. And I didn't learn a thing until I was introduced to the EGT and squirrely wiles of 2 cycles when I upgraded to Kolb Firestar.. It is my opinion that the lack of that instrument and the prolific use of 2 cycles in the early days and even today, has turned the reputation of Cuyuna into .....hmmmm, ..... something really bad. Of course the ASI is extremely important although I have flown a Pterodactyl for months without one, but there again, just like the long EZE, it wouldn't stall either, due to the variable angle of attack on the wing design and the fact that it was a canard. just a thought, and a lil nudge for the importance of EGT ... especially on 2 cycles. George Randolph Firestar driver from The Villages, Fl Rotax 447, 3 blade Ivo, KX, 1991 ________________________________________________________________________________
From: "David Key" <dhkey(at)msn.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
>From: "John Hauck" <jhauck(at)elmore.rr.com> >Reply-To: kolb-list(at)matronics.com >To: >Subject: Re: Kolb-List: RE: Flying without instruments??? >Date: Mon, 5 Dec 2005 19:28:51 -0600 > > > | Personally, if I were allowed one and only one flight instrument in >my >| airplane it'd be an altimeter. Altitude is the hardest to judge >without a >| gauge. The rest should only be nice to have in a light aircraft, >and >| _never_ essential for flight.... >| >| JMHO, >| >| LS >| N646F > >Hi LS/Gang: > >Reckon I'll have to disagree with this one too. ;-) > >Personally, I can see the ground a hell'uva lot easier than I can see >stall speed. Stall speed is much more important than knowing how high >I am, in my own humble opinion. > >Even is an air speed indicator is not calibrated accurately, it will >always indicate the same stall speed, no matter what altitude. > >From my poor memory, most Kolb fatal accidents are the result of >stalls low to the ground. Folks forget to cross check their airspeed >indicators, or they rely on their "instincts" to keep them above stall >speed. Very, very difficult to determine accurate airspeed by the >seat of the pants, especially when turning down wind at very low >altitudes. > >john h >MKIII/912S >hauck's holler, alabama > > ________________________________________________________________________________
From: "Don Gherardini" <donghe@one-eleven.net>
Subject: Re: RE: Seat-of-the-Pants/No Instruments???
Date: Dec 06, 2005
George.... When you said.. "" It is my opinion that the lack of that instrument and the prolific use of 2 cycles in the early days and even today, has turned the reputation of Cuyuna into .....hmmmm, ..... something really bad."" You explain a very important thing... IN those early days...we were NOT using ROTAX engines.....and we were not useing insturments....or at least very few insturments and least of which were engine monitoring. We used about every other engine that was light...MCCullochs, West Bends, Chryslers, and of course...the venerable Cuyuna. Dont know if I remember ANY of them being immune to our lack of knowledge about 2-strokes and prop-loading and the ..." squirrely wiles of 2 cycles "...as you so eloquently put it. I hate to admit it, but I tore up several without any regard to what brand they were. IT was not until I started useing engine monitering insturments did the rate of failure go down. At least as soon as I learned what was going on in that cylinder! AS I remember....it was a tach first.....then EGT.....or maybe CHT ...I dont really remember..but soon...nothing I built was without both heat monitering devices. I dont think these insturments keep me from gaulding cylinders so much as they just told me what I was doing to cause it to happen. They gave me a direction to go in tuneing the engine/carb/prop to keep it from happening again..or maybe I should say...as often! ANyway...your observations as usual....are right on the money I think. Don Gherardini OEM.Sales / Engineering dept. American Honda Engines Power Equipment Company CortLand, Illinois 800-626-7326 ________________________________________________________________________________
From: snuffy(at)usol.com
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
> The difficulty here is that stall is determined by _AOA_ and not airspeed. My entire takeoff roll with my Minimax I leave the tail on the ground so my AOA stays the same from zero to liftoff airspeed. According to your thesis, the wing wasn't ever stalled from the moment it started rolling forward. Do not archive ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
If my shaky memory serves me correctly, a stalled condition exists when the angle of attack is such that the airflow separates from the wing and it stops flying. In your case of takeoff, the wing probably isn't stalled, there simply isn't sufficient airflow to lift the plane off the ground. A similar case could be when coming in for landing at too low an airspeed, but good angle of attack. The plane wouldn't stall, but your rate of descent would be very high because of insufficient lift. Lots of bent gear from that one. Lar. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: <snuffy(at)usol.com> Subject: Re: Kolb-List: RE: Flying without instruments??? > >> The difficulty here is that stall is determined by _AOA_ and not > airspeed. > > > My entire takeoff roll with my Minimax I leave the tail on the ground so > my AOA stays the same from zero to liftoff airspeed. According to your > thesis, the wing wasn't ever stalled from the moment it started rolling > forward. > > Do not > archive > > > ________________________________________________________________________________
Date: Dec 06, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Re: RE: Flying without instruments???
> >Again, not to beat the dead horse, but I very respectfully and strongly >disagree with this. The airplane will tell you when you're approaching the >critical AOA in circumstances where the ASI won't be reliable. This works >every time, no matter what the wind is doing or how high you are. I think >it's absolutely critical that a pilot be trained to recognize these signs >and be able to fly accordingly. If you need the ASI to tell you you're >approaching the critical AOA, then I submit more training/experience in the >plane is needed. > >I should mention that this works perfectly for me in my FS II and I've never >stalled it inadvertantly as a result. My ASI is, well, less than accurate >I'll put it that way, especially in high AOA situations.... > >Ok, I'll stop now I promise. > Lucien, During relatively quiet flying conditions, the eyes on the horizon, the lower cheek and stick hand pressure give good feedback signal inputs. It is much like flying a sailplane with noise added. Now comes the but. But during cold winter days flying through very unstable air when the FireFly is bobbing and twisting like a fishing cork, it adds a high degree of distraction or error signal inputs that mask the good feedback signal inputs. This is especially true if your shoulder belts are less than snug. This is when I use the ASI. After flying sailplanes for a couple of years with hours of slow flight, I developed a response that when anything felt uncomfortable to push the stick forward. This reaction has carried over to the FireFly. In unstable air, I used to feel very uncomfortable turning from downwind to base and I would want to push the stick forward. This lead to getting beat up more than necessary by making a wider skidding turn. The addition of an elevator position indicator helped. I discovered that as I was being beat up in the turn, that if I kept the stick in the zero to one degree elevator up position, I could bring the FireFly on around with confidence and the discomfort disappeared. One may say that you should not fly in these kinds of conditions. But if you want to fly in the winter time, you have to endure unstable air when leaving and returning to altitude. Also, I use the ASI just after I flare the FireFly. A quick glance tells me how much time I have to nurse it on down before it quits flying. I credit ASI use as the major reason the landing gear legs on the FireFly have not been replaced. The other time I use the ASI is after lift off to establish climb rate. Yes, you can and should be able fly without instruments, but with them and their proper use, the risk to pilot and craft is reduced and the pilot flight envelope is increased. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
From: "c b" <seedeebee(at)hotmail.com>
Subject: 912 Kill Switch & Ignition Wiring
Date: Dec 06, 2005
Hey Fellow Kolbers, Well I've been working on my Mk III for 3 months now since the original exhaust system cracked up. I've got a new Titan Aircraft stainless system on the 912 - it looks awesome! While the ship was in dry dock, I decided to upgrade the kill switch, which seems to have resulted in a downgrade... Originally, there was a single switch that interrupted a wire that ran directly from the battery to the "L" and "R" terminals on the back of the ignition switch. When I hit the kill switch, the engine ran rough, but kept on running. So I decided that I would install 2 switches, one for each mag, and hook them up so they completely killed the engine. I removed the wire from the battery and wired in my switches to the wires that lead out from the "L" and "R" posts on the ignition switch. Now the engine runs rough all of the time, and the two kill switches do absolutely nothing. I looked in the Rotax install manual, and it doesn't make much sense to me. I can't find a diagram from which I can tell what I did wrong... I'm no wiring expert, but I didn't think I was a complete moron either... Any help would be greatly appreciated! Thanks! Chris Banys Kolb Mk III 912UL (will be amphib again in 2006) N10FR ________________________________________________________________________________
From: snuffy(at)usol.com
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
> > That's correct - if the wing section was not above the critical AOA with > respect to the relative wind, it wasn't stalled.... I'm glad to see you considered the relative wind . Does this relative wind have a velocity? If so is this wind velocity a factor in the flight of the wing? Or can we just fly this wing at any velocity as long as the wing is at the proper AOA? Do not archive ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
>I'm glad to see you considered the relative wind . Does this relative >wind have a velocity? Yes. > If so is this wind velocity a factor in the flight of >the wing? Yes. >Or can we just fly this wing at any velocity as long as the >wing is at the proper AOA? We can fly the wing as long as it generates enough lift to overcome gravity (hint: even a stalled wing still generates lift).... LS N646F >Do not >archive > > ________________________________________________________________________________
From: "J W Hauck" <jimh474(at)earthlink.net>
Subject: Re: RE: Flying without instruments???
Date: Dec 06, 2005
Lucien: Wut you be aviatin, de dang space shuttle? Jim Hauck Do not archieve ________________________________________________________________________________
Date: Dec 06, 2005
From: possums <possums(at)mindspring.com>
Subject: Flying without instruments???
I worked up a simple, inexpensive directional indicator on the top of my nose cone. Not only can I tell if the plane is slipping ..... if the little arrow is pointing back towards me, then I know my AOA is all wrong. Works every time. http://www.matronics.com/photoshare/possums@mindspring.com.09.27.2003/Seat2.jpg BTW the ole timers who first flew airmail would carry pigeons with them. The idea was to release one if they were caught in the clouds or the fog and follow the bird out. The problem was the pigeon didn't know which way was up either. http://www.matronics.com/photoshare/possums@mindspring.com.07.26.2002/thum.jpg >*I worked up a simple, inexpensive, and light weight aoa indicator that might >be of interest to anyone who flies a Kolb with the small nose cone. I have >been using it for last few months and it works well. > >It can be seen at: > >http://www.thirdshift.com/jack/firefly/firefly84.html > >Jack B. Hart FF004 >Jackson, MO* ________________________________________________________________________________
From: "pat ladd" <pj.ladd(at)btinternet.com>
Subject: Re: RE: Flying without instruments???
Date: Dec 07, 2005
Spent lots time tight turns ,>> Hi, I think all pilots in a perfect world would train in gliders. An average glider pilots flight, banked at 40 degress about 5 knots above the stall with 20 other gliders withing 400 yards all doing the same thing would give the average power pilot the screaming habdabs. Certainly gave me the habdabs sometimes. Cheers Pat -- ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: John W's Texas Flight Report
Date: Dec 07, 2005
http://home.comcast.net/~kolbrapilot1/2005_Flights/gky-mfe_2005.htm ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: John W's Texas Flight Report
Date: Dec 07, 2005
Very nice. Thanks..............envy rules. :-) Do not Archive. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "John Hauck" <jhauck(at)elmore.rr.com> Subject: Kolb-List: John W's Texas Flight Report > > http://home.comcast.net/~kolbrapilot1/2005_Flights/gky-mfe_2005.htm > > > ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: Re: RE: Flying without instruments???
Date: Dec 07, 2005
Look here for the "homemade" version of the high dollar "Lift reserve indicator". http://www.snyder.on.ca/pages/lri.htm This is a kind of "Ford vs Chevy" debate and some will just find this useless. I have talked to others that will swear by the AOA gauge as a landing aid. Have been told the U.S. Navy use AOA instrumentation heavily (they are arguably the most EXTREME short field landing pilots in the world ;-) Your mileage may vary... Jeremy Casey ________________________________________________________________________________
Date: Dec 07, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Home Made AOA Meter
> >Look here for the "homemade" version of the high dollar "Lift reserve >indicator". > Jeremy, This is great. One can get a little better printout from: http://www.ch601.org/resources/aoa/aoa.htm and the drawing prints out well from: http://www.ch601.org/resources/aoa/print/angleattack.jpg I changed the subject line. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
Date: Dec 07, 2005
From: Michael Deegan <kb7mxu(at)mindspring.com>
Subject: Mark III Xtra in Northwest?
Hi folks, first time post. I'm a novice pilot going for my Sport Pilot rating. The Mark III Xtra is on my short list of planes I might want to build, but I haven't seen one in the flesh yet. Does anyone in the group know of one flying in the Northwest, more specifically the Eastern Wash./North Idaho area? Could anyone contrast and compare the M3X with the Titan II and the RANS S-12 Airaile? I prefer the looks of the Kolb to either of these and the wing folding feature is good, but the taildragger aspect worries me a bit. but if the enthusiasm of the list members is anything to go by, these must be great planes. Thanks. Mike Deegan ________________________________________________________________________________
From: "pat ladd" <pj.ladd(at)btinternet.com>
Subject: Re: Downwind turns
Date: Dec 08, 2005
downwind turn close to the ground,without an airspeed indicator.>> Hi All, I can see this heading for the old arguement about airspeed decreasing as you turn down wind and I won`t go there, it has been done to death but I will make the point that if you are turning while low you are also flying into the area where the windspeed decreases because of its proximity to the ground. Remember `wind gradient` from those early lessons? Taking the extreme case. Iif you are flying (foolishly) only 5knots above the stall and the wind drops by 5 knots. Thats it. Kaput! With no height to recover. In stronger winds the gradient may drop by 10 or more. Cheers Pat -- ________________________________________________________________________________
Date: Dec 07, 2005
From: "David L. Bigelow" <dlbigelow(at)verizon.net>
Subject: RE: Flying without instruments
At the risk of beating this thread to death....... There's no doubt that a good angle of attack instrument is the best speed instrument available. Unfortunately, it's not practical for an ultralight (or any other a/c) unless it is amplified. You just can't see the difference between 10 and 12 degrees on a vane, and that's roughly where you will be flying on approach. Only aircraft I've ever flown without an airspeed indicator is hang gliders. Being completely exposed to the breeze, and able to hear every nuance of sound makes it easy to control airspeed. Also, hang gliders have a very positive hands off trim point, and it takes a fair amount of forward pressure on the control bar (think back stick) to stall one. Put yourself in a very noisy cockpit sheltered from the wind in an airplane with light stick forces, and it becomes very difficult to control airspeed precisely without an instrument reference. If I had to choose only one instrument, it would be the airspeed indicator. It's not a bad idea to practice stabilized approaches without looking at the airspeed indicator just in case you ever lose it, but as regular thing - good way to bust your rear. Dave Bigelow Kamuela, Hawaii FS2, DCDI 503 ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Last Flight 2005 - Texas
Date: Dec 08, 2005
Morning Gang: Had a good flight out to Texas to spend time flying with friends. Departed my airstrip, Gantt International Airport, 1000, 1 Dec 05. Dropped in on Paul Petty's in-laws, Harris Field, MS, for coffee and lunch. Next stop was John Bickham's new airstrip, Nauga Field, St Francisville, LA. John and his wife graciously put me up for the night after feeding me the best red beans and rice, and country sausage, I have ever eaten. In the process got to make the first landing and take off from John's airstrip. Next stop was Beaumont, TX. Didn't take long to fly there from St Francisville, LA. My ground speed was 115 mph. Airspeed was 85 mph. Would have been difficult to determine airspeed without my trusty Winter ASI. Don't know what my AOA was. ;-) Got on the ground and found my three friends had already arrived. John W on the left, Ken K middle, and Gary H, on the right: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3146_resize.JPG After lunch at Sonic we took off and headed for Port Authur, TX, the Texas/Louisiana State Line and the Gulf of Mexico. Here's John W and his Kolbra heading south on the Texas beach: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3145_resize.JPG Doing what we do best, low level down the beach from Louisiana to the Mexican Border. Shot of Gary H in his MKIII: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3149_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3150_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3153_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3155_resize.JPG John W's Kolbra: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3157_resize.JPG John W's Kolbra and Ken K's Titan: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3164_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3165_resize.JPG John W and Ken K leading Miss P'fer: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3174_resize.JPG The rest of the flight. All aircraft powered with the 912ULS. Might add, we had nary a problem aircraft or power-wise: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3177_resize.JPG Gary H and John W: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3182_resize.JPG The flight has to gain a little altitude and shift to maintain clearance with beach traffic: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3187_resize.JPG Good time was being had by all: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3193_resize.JPG Gary H approaches an old steel light house: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3195_resize.JPG John H gets a quick snapshot of the old steel light house on the fly: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3196_resize.JPG Shrimp boat ship wrecked on the beach: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3197_resize.JPG Made it down to Mustang Beach near Corpus Christi to RON. After a great steak dinner in the Yacht Club next to the air port, we sacked out on the floor of the FBO. Next morning after a short walk to the local convenience store for coffee and donuts, we were off to continue our flight down the beach. Here's Gary H leading the way: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3201_resize.JPG Perfect morning to be flying the beach, except we had a strong headwind. Air was smooth as silk coming off the water: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3202_resize.JPG This leg turned out to be 3.5 hours from Mustang Beach to McAllen, TX. Here are the guys just after we turned west up the Rio Grande River. That's Mexico on the other side. Gary called Brownsville Tower to get permission to fly through their airspace south of the field: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3203_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3204_resize.JPG We landed at Del Rio, TX. Last time I landed here was on the way to Alaska in 1994. Put up our tents and headed out walking to town for dinner. Found a local Mexican Resturant (really a locals place to eat) and had some excellent Mexican food. On the way back to the airport, stopped off at Dairy Queen for some ice cream to simmer in the recent Mexican dinner. It was still early when we got back to the airport, so we sat around and reminiced about the days flying: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3209_resize.JPG Next morning, Sunday, 4 Dec 05, we took off, headed west to the Rio Grande. Flew up stream until we came to the Pecos River. Turned right up the Pecos for a good ways, then headed for Sonora, TX: http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3210_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3213_resize.JPG http://www.c-gate.net/~ppetty/Hauck's%20Stuff/Last%20Flt%2005%20TX/DSCF3214_resize.JPG After a good Texas Sunday lunch buffet, our group split up. John W and Ken K headed for Arlington, TX. Gary H and I headed for Houston and his airstrip at Dry Creek. We made one quick op stop at Austin. The weather started turning cold and overcast. Up until this point we had been blessed with beautiful warm weather. Gary H and his wife feed me some Texas chilli and put me to bed. Next morning I was off for Alabama at 0830, 5 Dec. Got fuel in Natchez, MS. Didn't take time to eat lunch. If I had, I would not have been able to make Gantt IAP before dark. The weather was really cold now, 35 to 40F. After my fuel stop I was also sitting in the shade of the wing for the remainder of the flight back to Alabama. Had the Chilli Vest (12VDC) on WOT and still had cold feet and hands, despite wool socks and boots, and gloves. First time I had the thermostat on the jacket WOT and still colder than I ever got on two previous trips with the Chilli Vest to Alaska. However, I was dressed appropriately for the Alaska flights, and this flight I lacked some essential clothing. Flew five days straight. 2,429.6 sm. Average ground speed was 82.5 mph. Max ground speed was 124 mph. Burned 166.0 gal fuel at 5.4 gph. Might add Gary H and I both pushed our 912ULS's to keep up with the Kolbra and Titan. I flew 5,200 rpm most of the time, yielding 90 mph cruise. Was a great flight. We all had fun flying and visiting. Now it is time to get back to my chores. Won't be another good flight until next Spring. john h MKIII/912ULS Titus, Alabama ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Kolbra info
Date: Dec 08, 2005
Hi all, Not to take away from the airspeed/AOA thread, but.... ;) Are there any Kolbra builders/flyers on the list? The Kolbra is one of the planes I'm considering for my next plane, but I've searched up and down the internet in vain for detailed photos, info and etc (does Kolb make this plane anymore?)... In fact the Kolbra looks like just the ticket for my #1 airplane requirement (good view) because of the tandem seating...... I'd be interested to hear about it from other Kolbra owners/builders/flyers... Thanks, LS N646F ________________________________________________________________________________
From: "JIM HEFNER" <hefner_jim(at)msn.com>
Subject: Re: Home Made AOA Meter
Date: Dec 08, 2005
Jack, folks, This is exactly the setup my friend has implemented on his Zenith 701... this was a big topic of discussion on the Zenith thread not all that long ago, so he decided to implement on his plane and it is slick!! Having this instrument in the dash where it is readily visible during landing is great. Looking off to the side during landing is not a good thing, as Lucien indicated. Planes, including ultralights, that are in the business of towing gliders pretty much all use AOA meters of some sort, including strings out in the airstream, with a reference marker for stall AOA. For us casual Kolb fliers, I don't think this is an essential instrument, but if you are pushing the envelope with your Kolb, you might want to consider this. BB, I don't think I would go as far as saying this is more useful than a VSI, at least for my usage. I put a VSI in my FF early on and find myself using it a lot during flight... I have an adjustable trim tab, so it's nice to know I'm flying level while I'm trimming the plane out. Also on longer flights I find myself climbing or descending slightly when I didn't intend to... The LRI or AOA indicator would probably not get used near as much as my VSI. The FF with full flaps and ASI 50 lands great every time, so I'm not looking for more precision than that and I don't push the envelope with 90 degree banked turns at low altitude, so I doubt if this instrument would be all that useful to me. With folding the wings each time I fly, it would be tough to implement the LRI in the dash, with sender unit out under the wing, without a veryy long feeder tube fed through the rear wing mount/universal joint area, fed forward to the mounting location under the wing chord. Bottom line is, this started out as a technical discussion about ASI being the all truthful instrument, but it is not in all circumstances, where the AOA/LRI indicator is always valid. From a practical point of view, I think it is a neat concept, but I won't be implementing one on my FF anytime soon. Jim Hefner Tucson, AZ FF #022 > >Look here for the "homemade" version of the high dollar "Lift reserve >indicator". > Jeremy, This is great. One can get a little better printout from: http://www.ch601.org/resources/aoa/aoa.htm> and the drawing prints out well from: http://www.ch601.org/resources/aoa/print/angleattack.jpg> I changed the subject line. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
From: "Christopher Armstrong" <tophera(at)centurytel.net>
Subject: 914 turbo + 912uls=how much power
Date: Dec 08, 2005
HI experts, I have been looking at the specs of the Rota flat 4's and was wondering something. The 912 makes 80 hp at 5500 rpm with a Bore: 79.5 mm Stroke: 61 mm. Displacement: 1211 cu.cm (Compression: 9:1 Engine Weight: ~135 lbs The 912ULS makes 95 hp at 5500 rpm continuous (100hp at 5800 5 min max) with a Bore: 84mm Stroke: 61 mm. Displacement: 1352 cu.cm Compression: 9:1 Engine Weight: ~140 lbs The 914 UL2 makes 100 hp at 5500 rpm continuous (115 hp at 5800 5 min max) with a Bore: 79.5 Stroke: 61 mm. Displacement: 1211 cu.cm (Compression: 9:1 Engine Weight: ~167 lbs So if you add a similar sized turbo to a 912s what kinda power will you get? 912 goes from 80 to 100 (115 takeoff) so would a 912s go from 95 to 115 with 130 takeoff. At a weight of around 170 pounds that would be a decent engine. Add fuel injection while your at it and you have a real engine! Topher ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 914 turbo + 912uls=how much power
Date: Dec 08, 2005
Hi Topher/Gang: Not an expert, by any means. I get my info off the Kodiak web page. | The 912 makes 80 hp at 5500 rpm with a Bore: 79.5 mm Stroke: 61 mm. | Displacement: 1211 cu.cm (Compression: 9:1 Engine Weight: ~135 lbs 912UL makes 79 hp max continuous at 5,500 and 81 hp for 5 min max at 5,800 rpm. Engine w/gear box (an integral part of the engine) weighs 121.3 lbs. You can go to this page to add up accessory weight and add it to engine weight for all up flyable weight. Max torque is at 4,800.
http://www.kodiakbs.com/4intro.htm | The 912ULS makes 95 hp at 5500 rpm continuous (100hp at 5800 5 min max) with | a Bore: 84mm Stroke: 61 mm. Displacement: 1352 cu.cm Compression: 9:1 Engine | Weight: ~140 lbs 912ULS makes 95 max continuous at 5,500 and 100 hp at 5,800 rpm for 5 min max. Compression ration is 10.5 to 1, rather than 9.5 to 1 on the 912ULS. Eng w/gearbox weight is 124.8, not including accessories. | The 914 UL2 makes 100 hp at 5500 rpm continuous (115 hp at 5800 5 min max) | with a Bore: 79.5 Stroke: 61 mm. Displacement: 1211 cu.cm (Compression: 9:1 | Engine Weight: ~167 lbs | So if you add a similar sized turbo to a 912s what kinda power will you get? I can't answer that question. However, I, as well as John W, have discovered we do not need a turbo to get more power from the 912ULS, even at altitudes up to 15,000 feet. | 912 goes from 80 to 100 (115 takeoff) so would a 912s go from 95 to 115 with | 130 takeoff. Don't know that either. At a weight of around 170 pounds that would be a decent | engine. Add fuel injection while your at it and you have a real engine! For those of us with some "decent" hours flying with the 912UL and the 912ULS, we "know" we have a great engine. Would be extremely nice to have fuel inject, and I believe that we will see this improvement soon. BTW my max continuous cruise with the 912ULS is 95 hp @ 5,500 rpm, compared to 100 hp on the 914 at same rpm. The degradation of power at altitude has not presented a problem to those that fly regularly over the Rockies, and other mountain ranges. Take care, john h MKIII/912ULS hauck's holler, alabama ________________________________________________________________________________
From: Kirby Dennis Contr MDA/AL <Dennis.Kirby(at)kirtland.af.mil>
Subject: Kolb vs. Titan, Airaile
Date: Dec 08, 2005
Mike Deegan wrote: << Could anyone contrast and compare the M3X with the Titan II and the RANS S-12 Airaile? I prefer the looks of the Kolb to either of these and the wing folding feature is good, but the taildragger aspect worries me a bit... Thanks. >> Hi, Mike - Welcome to the List! You'll discover a wealth of info from the members here. Before I purchased my Mark-III kit, I visited Randy Schlitter's RANS factory in Hays, Kansas and flew with him in his 912-powered S-12 demonstrator. Nice plane, but I preferred the taildragger aspect of our Kolbs. The RANS kits have "prettier" hardware (like the brackets, rudder pedals, control horns, bellcranks, handles, etc.), which may suggest quality parts and good attention to details. Flies just like you'd expect a nosewheel Mark-3 to behave - very easy to fly. Construction is similar to a Kolb (aluminum tube & fabric). I think the S-12 is about 10 mph faster than a similarly-equipped Mark-III, because it is a bit more aerodynamically clean. But it's not as STOL-capable as the Mark-III, which is another feature I prefer on the Kolb. Everything is a tradeoff. The mild taildragger manners of a Kolb make 'em easy to master - not like many other tailwheel airplanes that are squirrly or difficult to control. But regardless of all those niceties on the RANS, my choice was more influenced by the wing-fold and transportability ease of our Kolbs, the robust quality of the Kolb kits, and the structural crashworthiness (read SAFETY) inherent in the Kolb design. And, Kolb Factory support is without doubt the best in the business! (see my List post of 6 Dec 05). I have no experience with the Titan, other than I know they are all metal and are a helluva lot faster than a Kolb on the same power. But again, the tradeoff is: it is way less STOL than a Kolb. (John Williamson's flying buddy Ken just finished a Tornado - maybe John can offer some direct comparisons with a Kolbra!) Pick the Mark-III. I love mine - no regrets that I didn't purchase something else. Dennis Kirby s/n M3-300, 1996 model, 912ul, 37.7 hrs total time, in Cedar Crest, NM ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 914 turbo + 912uls=how much power
Date: Dec 08, 2005
|I wonder if someone | were to buy the 914 would be getting the old engine with a turbo on it ? | Michael Bigelow Michael B/Gang: The 914 is based on the 912UL engine. No change to basic 912UL. Only difference between 912UL and 914 is the addition of turbo and supporting hardware. The 912ULS is the result of user testing for many years. As of January 2000, it was the result of 7,000 912 engines and 13 years user testing. It is a huskier cleaned up 912 with more displacement and compression. The 912 was a great engine. I put 1135 hour on mine before I got a chance to trade it for a 912ULS. Had no problems with the 912. It was 20% more economical that the 912ULS, ran a lot cooler, and both are equally reliable. My new 912ULS now has 1,098.1 hours on it. Runs as good as new. john h MKIII/912ULS ________________________________________________________________________________
From: WillUribe(at)aol.com
Date: Dec 08, 2005
Subject: Monument Valley 2006
Hello All, I have been looking into the 2006 flying season and need to know if there is any interest in another Kolb Gathering at Monument Valley. It looks like 19-21 May should be the proper time to get together at Monument Valley. 23-24 May would also be a good time to gather on the floor of the Alvord Desert again if anyone is interested. I am planning on being at both places then on out to the Oregon coast, then fly south along the California coast before coming back home. If I have missed anyone in the address line, please pass this information on to them and as always, invite whoever you would like to gather with us. John Williamson Arlington, TX Kolb Kolbra, Rotax 912ULS, 1006 hours http://home.comcast.net/~kolbrapilot1 kolbrapilot2(at)comcast.net ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Monument Valley 2006
Date: Dec 08, 2005
| I'm new to the list, but am getting the impression that this is a | regular/yearly thing for kolbers? Yep, we do it every year. Started the first Unplanned/Unorganized Kolb Flyin three years ago. The 2006 MV Flyin will be number 4. "Do you fly up there or do you trailer?" I never trailer. Some folks do trailer in. Come any way you desire. This is a very informal get together of some great folks, not including me. ;-) | Also, I can't seem to access any of the links on your site, they all give me | "page not found". Don't know what to tell you about the links. They work for me. john h MKIII/912ULS Titus, Alabama ________________________________________________________________________________
From: DAquaNut(at)AOL.COM
Date: Dec 08, 2005
Subject: Re: Prop noise
John, I wonder how ,or if it changed the flight characteristics top speed etc Ed (in Houston). In a message dated 12/4/2005 9:32:54 A.M. Central Standard Time, jrjungjr(at)yahoo.com writes: Group, Yesterday, I flew for the first time after raising the engine up a full inch, leaving a 2 inch gap between the prop tip and the boom tube. It was noticeably quieter, than with only 1 inch of clearance. John Jung ________________________________________________________________________________
From: DAquaNut(at)aol.com
Date: Dec 08, 2005
Subject: Re: Hanger
In a message dated 12/4/2005 10:09:09 A.M. Central Standard Time, gittj(at)earthlink.net writes: Trailer is fine but you need two people and it is a pain and some times hard to find that other person to help out . Aviation needs to make a nother step forward, in a new designe . Kolb is a great little plane i really enjoy mine but it sure would be nice to drive it home ,not paying hanger rent and work on it when i had time at home . For what it's worth! { Dreamer } Larry Larry, I have never had anyone to help me with my Firefly folding. Care must be taken but it can be done by yourself if its not to windy and you make a few fixtures to protect the ends of the wings. Ed ******** Do Not Archive ********** ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Prop noise
Date: Dec 09, 2005
Ed and Group, I flew for more than a year with the engine raised 3/4 inch, and never noticed any difference in flight characteristics or top speed. John Jung Firestar II N6163J Surprise, AZ On Dec 9, 2005, at 12:56 AM, Kolb-List Digest Server wrote: > > > John, > > I wonder how ,or if it changed the flight characteristics top > speed etc > > Ed (in Houston). ________________________________________________________________________________
From: "pat ladd" <pj.ladd(at)btinternet.com>
Subject: Re: Monument Valley 2006
Date: Dec 09, 2005
Um, I don't think the Welsh are a "race"... besides, the word is "welch"...>> Hi Robert, hmm? Well, as the Welsh border is only about 30 miles from where I live I am not going to risk the Welsh starting their raiding into England again just to get at me if I annoy them I will leave that question alone. On the spelling......my Oxford Dictionary gives `Welch. Old spelling of Welsh retained in the name Royal Wech Fusiliers. My Longmans Contemporary English gives " welsh, welch. to avoid payment. as in 1 `he welshed on his bet` 2 to break ones word or promise. 3 she welshed on her promise` USAGE. This verb is considered offensive by Welsh people. You made me look it up though. Cheers Pat -- ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: English lessons ;-)
Date: Dec 09, 2005
Next thing you know that bloody Brit will try to tell us that airplane is supposed to be spelled "AEROplane"!!! (Tongue firmly and squarely planted in my cheek ;-) As someone once said, "The U.S. and the U.K., 2 countries separated by a common language... Jeremy "occasional visitor to the U.K." Casey My Longmans Contemporary English gives " welsh, welch. to avoid payment. as in 1 `he welshed on his bet` 2 to break ones word or promise. 3 she welshed on her promise` USAGE. This verb is considered offensive by Welsh people. You made me look it up though. Cheers Pat ________________________________________________________________________________
From: "J.D. Stewart" <jstewart(at)inebraska.com>
Subject: 912 vs 912S question
Date: Dec 09, 2005
91 is as good as it gets around here. J.D. > > > JD, > > Were you using 91 or 93 octane autogas with the 912 ULS? > > Jim > > Jim Pellien > Mid-Atlantic Sports Planes > www.MASPL.com > 703-313-4818 > jim(at)sportsplanes.com > > ________________________________________________________________________________
From: "Jeremy Casey" <n79rt(at)kilocharlie.us>
Subject: 912 vs 912S question
Date: Dec 09, 2005
J.D. I think he was trying to compare speed to speed, not RPM to RPM. The 912S turning the same RPM as the 912 should be going faster (i.e. doing more work) hence certainly should burn more gas. Do you remember what speed the 912 was doing at say 4900 and then compare what rpm the 912S has to turn to get the same speed (should be less RPM's...I think the question is if it will be less GPH) Jeremy Casey -----Original Message----- From: J.D. Stewart [mailto:jstewart(at)inebraska.com] Subject: RE: Kolb-List: 912 vs 912S question On my Titan SS, I started with a 912 for the first 6 hours, then switched over to a 912S, so I can offer a good comparison. Same plane, same rpm (4800~4900), I was getting 3.8gph with the 912, and am using 4.8gph with the 912S. It didn't hurt that the 912 used regular gas either, especially with the cost of gas now. J.D. Stewart UltraFun AirSports, LLC http://www.ultrafunairsports.com Challenger e-mail list http://challenger.inebraska.com Titan e-mail list http://groups.yahoo.com/group/Titanaircraft/ ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 912 vs 912S question
Date: Dec 09, 2005
| (4800~4900), I was getting 3.8gph with the 912, and am using 4.8gph with the | 912S. It didn't hurt that the 912 used regular gas either, especially with | the cost of gas now. | | J.D. Stewart JD S/John J/Gang: Looks good to me. my 912UL on MKIII at 5,000 rpm burned 4.0 gph my 912ULS on the same MKIII at 5,000 rpm burns 5.0 gph I didn't find out about the 912 using a minimum of 87 octane fuel until the weekend I traded it in to Ronnie Smith and attended the 912 school during the same weekend. Eric Tucker gave us that info after flying with 93 octane for 1,135 hours, when I could have been running the cheap stuff. Plugs last half as long in the 912S as the 912, also. john h MKIII/912ULS Titus, Alabama ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 912 vs 912S question
Date: Dec 09, 2005
| Were you using 91 or 93 octane autogas with the 912 ULS? | | Jim Jim/All: Minimum octane fuel for 912ULS is 91 octane. Kinda hard to find any place I have been in lower 48, canada, and alaska, so I opt for 93 when available. When not, I got for what the FBO sells, 100LL. john h ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Re: 912 vs 912S question
Date: Dec 09, 2005
> | Were you using 91 or 93 octane autogas with the 912 ULS? >| >| Jim > >Jim/All: > >Minimum octane fuel for 912ULS is 91 octane. Kinda hard to find any >place I have been in lower 48, canada, and alaska, so I opt for 93 >when available. When not, I got for what the FBO sells, 100LL. > >john h Hey John, that's interesting, I was thinking about a 912ULS for my next project if it should ever come to pass, but now that you mention this I might want to stick with a 912 (so I can use the cheaper 87 octane gas)... Also, why is the plug life shorter on the S? Thanks, LS N646F > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 912 vs 912S question
Date: Dec 09, 2005
| Also, why is the plug life shorter on the S? | LS LS/All: If I remember correctly from Eric Tucker and the 912 School, it is because of the higher compression ratio, 10.5 to over the 912UL 9.5 to 1. 912ULS runs hotter and is harder on plugs. That is about all the info I have on that subject. Based on 1,098.1 hours on my 912ULS, they are ready to come out at 100 hours. I have pushed them to 125 hours, as I did the 912 to 225 hours, just to see what they would do. No change in performance when replaced with new plugs in either model as far as I could determine. john h PS: The extra power of the 912ULS is a kick in the ass over the 912. Nice to have that extra power, even if I have to pay more for it. ;-) ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Thrust line change
Date: Dec 09, 2005
|We will be changing the thrust angle to | see if it helps. | Richard Pike Richard P/Gang: Experimentation was done on my Firestar and MKIII with little if no change. Not enough to really notice. Changed vertical and horizontal orientation of engine. Also experimented with changing the leading edge of the upper vertical stabilizer with not enough change to warrant messing with it. Designed and fabricated adjustable forward horizontal stabilizer mounts. Experimented with different settings to find the "sweet spot" for my airplane. The one thing I try to do on my airplane is keep the engine and thrust line as low as possible. The more power available to me, the more I want the thrust line low. I am no aerodynamic design engineer, but I believe the more the engine is moved from the center of mass on a pusher, the more power it is robbing to fly the aircraft. Imagine what a 40 inch off set would do to my MKIII if it was horizontal, and not vertical. Actually, the thrust line on my airplane is 36.75" inches from the top of the tail boom. I don't know where the center of mass is on my airplane. This gives me .75" clearance between prop tips and tail boom. Yes, the 72" prop seems to be louder in the cockpit than the previous 70" prop I was flying. The 70" prop gave me 1.75" clearance between prop tip and tail boom. Rather have less noise and more performance, but the pusher configuration on the Kolbs doesn't work that way. john h MKIII/912ULS ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: 912 vs 912S question
Date: Dec 09, 2005
| > my 912UL on MKIII at 5,000 rpm burned 4.0 gph | | At what airspeed? | | > my 912ULS on the same MKIII at 5,000 rpm burns 5.0 gph | | At what airspeed? Snuffy/Gang: I don't know. About the same. Maybe a little faster with the 912ULS. I'll say 80 mph for the 912UL and 88 for the 912ULS. Time is flying by so fast I can't keep up with it. Heck, been flying the 912ULS 6 years this Spring. john h MKIII/912ULS ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Thrust line change
Date: Dec 09, 2005
First line of previous should have read, "little or no" instead of "little if no" change. john h ________________________________________________________________________________
Date: Dec 09, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Re: Thrust line change
Agree with all you say, and we also have the prop tips (68" prop) less than 1" from the tube... but here's the situation - have noticed a difference in trim change with power settings, higher power requires more back stick, less power and the noses rises a bit, and since we are way over powered relative to the original design parameters - since we are using a 582 - and what was the Firestar originally designed for - a 447? (I really don't know) ... Anyway, here's my question: Are we more concerned with center of mass or center of drag? And which is more important? The thrust line relative to the center of mass or drag? I would think drag, at high speeds and high thrust situations. If all the thrust you have to work with is coming from a 447 or a 503, and it is relative to the center of drag instead of mass, I wonder if you have enough thrust available to get outside of what Homer and Dennis originally designed the Firsetar to have, and therefore, changing the thrust line with those engines (447/503) would not amount to much - On the other hand, with a 582, now you have more thrust than the designers planned for, so is it possible to adjust the handling characteristics for those situations which are now outside the original parameters by changing the thrust line? Don't know. But since all it takes is two bolts 3/8" longer than original, and a handful of flat washers, I guess we'll find out... Stay tuned, film at eleven... Richard Pike MKIII N420P (420ldPoops) At 06:43 PM 12/9/2005, you wrote: > > >|We will be changing the thrust angle to >| see if it helps. | Richard Pike > >Richard P/Gang: > >Experimentation was done on my Firestar and MKIII with little if no >change. Not enough to really notice. Changed vertical and horizontal >orientation of engine. > >Also experimented with changing the leading edge of the upper vertical >stabilizer with not enough change to warrant messing with it. > >Designed and fabricated adjustable forward horizontal stabilizer >mounts. Experimented with different settings to find the "sweet spot" >for my airplane. > >The one thing I try to do on my airplane is keep the engine and thrust >line as low as possible. The more power available to me, the more I >want the thrust line low. I am no aerodynamic design engineer, but I >believe the more the engine is moved from the center of mass on a >pusher, the more power it is robbing to fly the aircraft. Imagine >what a 40 inch off set would do to my MKIII if it was horizontal, and >not vertical. Actually, the thrust line on my airplane is 36.75" >inches from the top of the tail boom. I don't know where the center >of mass is on my airplane. This gives me .75" clearance between prop >tips and tail boom. Yes, the 72" prop seems to be louder in the >cockpit than the previous 70" prop I was flying. The 70" prop gave me >1.75" clearance between prop tip and tail boom. Rather have less >noise and more performance, but the pusher configuration on the Kolbs >doesn't work that way. > >john h >MKIII/912ULS > > ________________________________________________________________________________
From: HShack(at)aol.com
Date: Dec 09, 2005
Subject: Re: Thrust line change
In a message dated 12/9/2005 9:13:51 PM Eastern Standard Time, richard(at)bcchapel.org writes: Are we more concerned with center of mass or center of drag? And which is more important? The thrust line relative to the center of mass or drag? I would think drag, at high speeds and high thrust situations. If all the thrust you have to work with is coming from a 447 or a 503, and it is relative to the center of drag instead of mass, I wonder if you have enough thrust available to get outside of what Homer and Dennis originally designed the Firsetar to have, and therefore, changing the thrust line with those engines (447/503) would not amount to much - On the other hand, with a 582, now you have more thrust than the designers planned for, so is it possible to adjust the handling characteristics for those situations which are now outside the original parameters by changing the thrust line? Don't know. But since all it takes is two bolts 3/8" longer than original, and a handful of flat washers, I guess we'll find out... Stay tuned, film at eleven... There is a seaplane that has the engine mounted very high in a pod on a pylon [I think it may be called a "Lake"]. To offset the very high thrust line, the engine is tilted to give up- thrust looks like about 20 degrees [this from memory]. We too have done some experimenting with various thrust angles with little results, but maybe we didn't go far enough. Maybe we needed to go twice as far as we did.............. Howard Shackleford FS II SC ________________________________________________________________________________
From: "Christopher Armstrong" <tophera(at)centurytel.net>
Subject: Thrust line change
Date: Dec 09, 2005
>>>To offset the very high thrust line, >>>the engine is tilted to give up- >>>thrust looks like about 20 degrees [this from memory]. According to Thurston ( designer of the Teal, which is the root of the Lake design) the cruciform tail was used to place it in the propwash, and the lift on the tail varies directly with power input to counter pitching effects due to power changes. I think you will find that the thrust line on these planes is lined up with the cruise attitude of the plane. Parked on the water they will look like they are pointing upwards a fair bit but when flying they will not. If you did alter thrust line on your Kolb to try to get it in line with the center of gravity , The pitching moment due to thrust is the thrust times the moment arm to the cg, not the Aero center. (Drag adds its moment as drag times its moment arm to the cg but it doesn't change with thrust setting, only with speed.) To change the thrust moment arm significantly would require so much angle to get the effect you want that it would be terrible for prop efficiency ( not to mention result in yaw due to the higher aoa and velocity on the prop on one side of the plane versus the other, p-factor in cruise is a very bad thing). The engine is fairly close to the CG front to back so you would have to tilt the engine many degrees to reduce the thrust line moment arm significantly. If the engine was farther back then only a bit of angle change would reduce the thrust moment arm much more. If you raise the engine too much the plane will not have enough pitch control to overcome the pitch due to thrust and you will not be able to rotate or climb. ________________________________________________________________________________
From: DAquaNut(at)AOL.COM
Date: Dec 10, 2005
Subject: Re: Trailers
In a message dated 12/9/2005 1:00:02 P.M. Central Standard Time, ulpilot(at)cavtel.net writes: I am interested in the ramp you have put in the center of the trailer. Do you have a picture you could send me? I had a FS KXP that I kept in the trailer and had to take the wheels off the trailer and raise the tongue in order to prevent from scraping the LE of the folded wings when unloading/loading down my ramp door. Thanks Jim Ballenger Jim, I built a dolly for my Firefly that cradles the tail wheel axle . It raises the tail wheel about a foot or so. This gives good clearance at the back where I need it most. The dolly holds the axle to where I can push the plane up the incline of the tilted trailer. the dolly can be made to lift the tail to what ever height you need. You might consider the advantage of using a dolly to gain a little height. I couldn't make it without mine. Ed ________________________________________________________________________________
Date: Dec 10, 2005
From: David Lehman <david(at)davidlehman.net>
Subject: Firestar Hauling...
Just when I thought I was smarter than the average bear and had this all figured out... I'm questioning my tail support... What is the distance from the leading edge of the wing to the bottom of the tail boom in the area forward of the tail with the wings folded?... If this was answered before, I'm sorry, I can't find it now... Less than two weeks before I pick her up, yeah, I'm excited!... Thanx... David ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: Trailers
Date: Dec 10, 2005
Jim, I'm not sure this is what you're looking for, but John Wood very neatly solved the leading edge problem in the trailer I bought from him. I had to modify it a bit to work with my truck, but it works very well. Take a look at my web page: www.biglar.homestead.com/landing.html I also have a winch in the front to pull my heavier Mk III up the slope. Lar. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "Jim Ballenger" <ulpilot(at)cavtel.net> Subject: Re: Kolb-List: Trailers > > Chris > I am interested in the ramp you have put in the center of the trailer. Do > you have a picture you could send me? I had a FS KXP that I kept in the > trailer and had to take the wheels off the trailer and raise the tongue in > order to prevent from scraping the LE of the folded wings when > unloading/loading down my ramp door. > Thanks > Jim Ballenger > MK III X 582 > Virginia Beach, VA ________________________________________________________________________________
Date: Dec 10, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Thrust line change
Kolbers, With the Victor 1+ belt reduction drive, it was possible to investigate what would happen if the thrust line was lowered. Using the same propeller setting and cruise rpm, the FireFly picked up about 0.6 mph for each inch the thrust line was lowered. You can check out how it was done at: http://www.thirdshift.com/jack/firefly/firefly56.html Also, I made some assumptions and calculated the change in FireFly wing and tail loads as the thrust line was changed. I guessed that the center of drag passed through the trailing wing attachment point and I assumed a CG near the aft limit. These calculations indicate that for level and for flight under identical conditions, for every inch the thrust line was lowered about one pound came off the wing and the tail. Also, if you move the CG forward the forward limit, lowering the thrust line is more productive. How it was done can be seen at: http://www.thirdshift.com/jack/firefly/firefly101.html I guessed at the center drag position. It seems that if the Firefly is symmetrical, the center of drag should be on the vertical center line. One way to get a better first guess would be to draw up the scaled front view profile, print it out on paper, cut out the profile and balance it on the point of a pin along a vertical line through the central axis. The balance point will be the center of flat plate drag. Scaling this point back up to real size should give a first guess as to where the actual center of drag is on the FireFly. Drove by the airport. They have plowed the apron and runways, but they have not plowed the taxi ways to and in between the hangars. The FireFly hangar doors are snowed shut. So today, it might be a good day to draw a front FireFly profile. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
Date: Dec 10, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Thrust line change
Got a question on your post, especially the last sentence - physically raising the engine too much relative to the airframe will obviously sooner or later get things to the point that the thrust line moment would overpower the control authority of the elevators, but I am considering shimming the rearmost motor mounts to raise the prop end of the engine. The goal is to reduce the need to retrim elevator pressure with changes in throttle settings. My thinking is, when the forward end of the engine is too high relative to the chordline of the wing, then the thrust line relative to both the center of drag and the center of mass requires various amounts of up elevator to counteract as throttle settings change. Because the thrust is trying to push the nose down. Raising the rear of the engine so that the thrust vector goes through the chordline of the wing ought to give opposite results, and surely does up to a point, but as I read your post, apparently you get to a place where changing the thrust vector to improve elevator pressure ceases to be helpful and only adds wierd side effects. Or are you talking thrust moment arm, and I am applying it to thrust vector angles? Or did I miss something? (Always likely...) Advice welcome - Thanks Richard Pike MKIII N420P (420ldPoops) At 12:16 AM 12/10/2005, you wrote: > > >The pitching moment due to thrust is the thrust times >the moment arm to the cg, not the Aero center. (Drag adds its moment as >drag times its moment arm to the cg but it doesn't change with thrust >setting, only with speed.) To change the thrust moment arm significantly >would require so much angle to get the effect you want that it would be >terrible for prop efficiency ( not to mention result in yaw due to the >higher aoa and velocity on the prop on one side of the plane versus the >other, p-factor in cruise is a very bad thing). The engine is fairly close >to the CG front to back so you would have to tilt the engine many degrees to >reduce the thrust line moment arm significantly. If the engine was farther >back then only a bit of angle change would reduce the thrust moment arm much >more. If you raise the engine too much the plane will not have enough pitch >control to overcome the pitch due to thrust and you will not be able to >rotate or climb. > > ________________________________________________________________________________
Date: Dec 10, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Thrust line change
> more. If you raise the engine too much the plane will not have enough pitch >control to overcome the pitch due to thrust and you will not be able to >rotate or climb. Chris & Richard, I have seen evidence of this with my FireFly. If I tease it off with three degrees of flaperon and stick back against the stop, the FireFly will fly off very nicely at minimum speed. But if I get aggressive with the throttle while using the same stick back and flaperon setting, the FireFly will accelerate well past minimum flight speed but it will not break loose until I drop the throttle back. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
Date: Dec 10, 2005
From: roger lee <ssadiver1(at)yahoo.com>
Subject: Thrust line change
Hi All, Just to let everyone know that Kolb has new horizontal stabilizer brackets that have a 4 position adjustment set up for trim. These new brackets take the place of the old stainless steel "L" brackets up front on the horizontal stabilizer. I just ordered a set so I will let you all know very soon. Right now I have to use too much trim to keep the nose of my Mark III Classic level. My nose wants to pitch down with the way they have it set up now. Roger Lee Tucson, AZ Richard Pike wrote: Got a question on your post, especially the last sentence - physically raising the engine too much relative to the airframe will obviously sooner or later get things to the point that the thrust line moment would overpower the control authority of the elevators, but I am considering shimming the rearmost motor mounts to raise the prop end of the engine. The goal is to reduce the need to retrim elevator pressure with changes in throttle settings. My thinking is, when the forward end of the engine is too high relative to the chordline of the wing, then the thrust line relative to both the center of drag and the center of mass requires various amounts of up elevator to counteract as throttle settings change. Because the thrust is trying to push the nose down. Raising the rear of the engine so that the thrust vector goes through the chordline of the wing ought to give opposite results, and surely does up to a point, but as I read your post, apparently you get to a place where changing the thrust vector to improve elevator pressure ceases to be helpful and only adds wierd side effects. Or are you talking thrust moment arm, and I am applying it to thrust vector angles? Or did I miss something? (Always likely...) Advice welcome - Thanks Richard Pike MKIII N420P (420ldPoops) At 12:16 AM 12/10/2005, you wrote: > > >The pitching moment due to thrust is the thrust times >the moment arm to the cg, not the Aero center. (Drag adds its moment as >drag times its moment arm to the cg but it doesn't change with thrust >setting, only with speed.) To change the thrust moment arm significantly >would require so much angle to get the effect you want that it would be >terrible for prop efficiency ( not to mention result in yaw due to the >higher aoa and velocity on the prop on one side of the plane versus the >other, p-factor in cruise is a very bad thing). The engine is fairly close >to the CG front to back so you would have to tilt the engine many degrees to >reduce the thrust line moment arm significantly. If the engine was farther >back then only a bit of angle change would reduce the thrust moment arm much >more. If you raise the engine too much the plane will not have enough pitch >control to overcome the pitch due to thrust and you will not be able to >rotate or climb. > > --------------------------------- ________________________________________________________________________________
From: "Christopher Armstrong" <tophera(at)centurytel.net>
Subject: Thrust line change
Date: Dec 10, 2005
Just changing the thrust angle itself does not change the pitching moment due to thrust, you must change the thrust moment arm to the cg. If you moved the engine up and tilted it at the same time to keep a constant moment arm to the cg then there would be no pitching moment due to thrust change. Tilting alone will change the pitching moment due to thrust by however much the moment arm changes. Unfortunately the cg of a Kolb is close to the engine. On a plane with the engine ten feet from the cg you could get a big change by tilting the engine a bit, but on a Kolb it is maybe 2 feet away. So spinning the engine a bit does not change the moment arm much. If the engine were on the cg then you could spin it all over and it would not change PM at all. There would be no pitching moment due to thrust! Course if you pointed the engine straight up (thrust straight down) there would be no thrust in the direction that you want either! In cruise flight you want the thrust pointed directly forward. If you don't then you end up shoving the plane sideways (well downways) through the air. If the plane is being shoved downwards through the air the wing and tail will be at different angles of attack and their contributions to pitching moment will change. So even if you didn't get a change in pitching moment due to thrust, turning the engine will result in a different total pitching moment, due to the wing, tail and fuselage going through the wind at a slightly different angle. All of you know you don't want to fly around in a sideslip, cause the plane just flys bad. Well you don't want to fly around with downslip or upslip either. The plane will be inefficient. The fuselage is designed (term used loosely when referring to a Kolb fuselage, they basically are cages that fit around the people and hard points, not very aerodynamic!) to fly through the air at cruise at a specific angle, and the wings, engine and tail are mounted on the fuselage to let the fuselage to fly at that angle in cruise, and the prop is designed to be perpendicular to the wind at that angle. If you tilt the engine more then a few degrees all of this will get screwed up and the plane will downslip or upslip. Would you fly around with the engine tilted to one side more then about 3 degrees, and force the plane to fly around in a sideslip? I don't think so. Christopher Armstrong -----Original Message----- From: owner-kolb-list-server(at)matronics.com [mailto:owner-kolb-list-server(at)matronics.com] On Behalf Of Richard Pike Subject: RE: Kolb-List: Thrust line change Got a question on your post, especially the last sentence - physically raising the engine too much relative to the airframe will obviously sooner or later get things to the point that the thrust line moment would overpower the control authority of the elevators, but I am considering shimming the rearmost motor mounts to raise the prop end of the engine. The goal is to reduce the need to retrim elevator pressure with changes in throttle settings. My thinking is, when the forward end of the engine is too high relative to the chordline of the wing, then the thrust line relative to both the center of drag and the center of mass requires various amounts of up elevator to counteract as throttle settings change. Because the thrust is trying to push the nose down. Raising the rear of the engine so that the thrust vector goes through the chordline of the wing ought to give opposite results, and surely does up to a point, but as I read your post, apparently you get to a place where changing the thrust vector to improve elevator pressure ceases to be helpful and only adds wierd side effects. Or are you talking thrust moment arm, and I am applying it to thrust vector angles? Or did I miss something? (Always likely...) Advice welcome - Thanks Richard Pike MKIII N420P (420ldPoops) At 12:16 AM 12/10/2005, you wrote: > > >The pitching moment due to thrust is the thrust times >the moment arm to the cg, not the Aero center. (Drag adds its moment as >drag times its moment arm to the cg but it doesn't change with thrust >setting, only with speed.) To change the thrust moment arm significantly >would require so much angle to get the effect you want that it would be >terrible for prop efficiency ( not to mention result in yaw due to the >higher aoa and velocity on the prop on one side of the plane versus the >other, p-factor in cruise is a very bad thing). The engine is fairly close >to the CG front to back so you would have to tilt the engine many degrees to >reduce the thrust line moment arm significantly. If the engine was farther >back then only a bit of angle change would reduce the thrust moment arm much >more. If you raise the engine too much the plane will not have enough pitch >control to overcome the pitch due to thrust and you will not be able to >rotate or climb. > > ________________________________________________________________________________
From: "Jim Ballenger" <ulpilot(at)cavtel.net>
Subject: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC VEST
TESTIMONIAL
Date: Dec 10, 2005
All A couple of weeks ago when the weather got cold here in Virginia I had trouble getting a satisfactory mag check. The manual states to run up to 3500 rpm and check each mag for no more than 300 rpm drop. During the hot summer months I was able to get good mag check with my needle set in the lowest position on my 582 blue head. When the temperature dropped into the upper thirties/lower forties I could not get my engine to turn more than 3000 rpm before it would bog down. I used the choke and it would turn up to 4000 rpm. Armed with that information I called Lockwood Aviation and they advised me to raise the needle in the carbs. I put my clip in the third notch from the top and it runs great. This is the first water cooled 2 stroke rotax I have owned and I am finding it somewhat different to tune than my prior 277/377/447 air cooled engines. I have also found out in the cold weather that I needed to install about 4 " of aluminum sheeting on the face of each radiator to keep the water temperature at least 150 degrees. This morning the OAT was 32 and I was able to keep my water temp at 152 with 5800 rpm. Since I have an electrical system on the MK III X and I had an electric vest left over from my motorcycling days, I took John Hauck's advise and hooked up the vest to the battery. What a great easy way to stay warm without all the hassles of installing a heater system. With the thermostat on 0/1 position I was warm and my voltage meter indicated a 13.2 volts so the vest did not take prevent the battery from being charged while I was flying. Thanks John. Jim Ballenger MK III X 582 Virginia Beach, VA ________________________________________________________________________________
Date: Dec 10, 2005
From: Richard Pike <richard(at)bcchapel.org>
Subject: Thrust line change
OK, we are on the same page. What you said is what I thought, so we agree. Question is, if the plane is in an upslip or downslip, then I would think a throttle setting change would change the stick pressure needed to maintain level flight - Consequently, what we need to do is accurately determine the angle of the wing relative to the airflow at level cruise. This could likely be done using a level and a set of marks, etc. Once this is properly determined, then we determine if the prop is vertical. Then we go from there. Richard Pike MKIII N420P (420ldPoops) At 04:14 PM 12/10/2005, you wrote: > > >Just changing the thrust angle itself does not change the pitching moment >due to thrust, you must change the thrust moment arm to the cg. If you >moved the engine up and tilted it at the same time to keep a constant moment >arm to the cg then there would be no pitching moment due to thrust change. >Tilting alone will change the pitching moment due to thrust by however much >the moment arm changes. Unfortunately the cg of a Kolb is close to the >engine. On a plane with the engine ten feet from the cg you could get a big >change by tilting the engine a bit, but on a Kolb it is maybe 2 feet away. >So spinning the engine a bit does not change the moment arm much. If the >engine were on the cg then you could spin it all over and it would not >change PM at all. There would be no pitching moment due to thrust! Course >if you pointed the engine straight up (thrust straight down) there would be >no thrust in the direction that you want either! In cruise flight you want >the thrust pointed directly forward. If you don't then you end up shoving >the plane sideways (well downways) through the air. If the plane is being >shoved downwards through the air the wing and tail will be at different >angles of attack and their contributions to pitching moment will change. So >even if you didn't get a change in pitching moment due to thrust, turning >the engine will result in a different total pitching moment, due to the >wing, tail and fuselage going through the wind at a slightly different >angle. > >All of you know you don't want to fly around in a sideslip, cause the plane >just flys bad. Well you don't want to fly around with downslip or upslip >either. The plane will be inefficient. The fuselage is designed (term used >loosely when referring to a Kolb fuselage, they basically are cages that fit >around the people and hard points, not very aerodynamic!) to fly through the >air at cruise at a specific angle, and the wings, engine and tail are >mounted on the fuselage to let the fuselage to fly at that angle in cruise, >and the prop is designed to be perpendicular to the wind at that angle. If >you tilt the engine more then a few degrees all of this will get screwed up >and the plane will downslip or upslip. Would you fly around with the engine >tilted to one side more then about 3 degrees, and force the plane to fly >around in a sideslip? I don't think so. > > >Christopher Armstrong > > >-----Original Message----- >From: owner-kolb-list-server(at)matronics.com >[mailto:owner-kolb-list-server(at)matronics.com] On Behalf Of Richard Pike >To: kolb-list(at)matronics.com >Subject: RE: Kolb-List: Thrust line change > > >Got a question on your post, especially the last sentence - >physically raising the engine too much relative to the airframe will >obviously sooner or later get things to the point that the thrust >line moment would overpower the control authority of the elevators, >but I am considering shimming the rearmost motor mounts to raise the >prop end of the engine. The goal is to reduce the need to retrim >elevator pressure with changes in throttle settings. > >My thinking is, when the forward end of the engine is too high >relative to the chordline of the wing, then the thrust line relative >to both the center of drag and the center of mass requires various >amounts of up elevator to counteract as throttle settings change. >Because the thrust is trying to push the nose down. > >Raising the rear of the engine so that the thrust vector goes through >the chordline of the wing ought to give opposite results, and surely >does up to a point, but as I read your post, apparently you get to a >place where changing the thrust vector to improve elevator pressure >ceases to be helpful and only adds wierd side effects. > >Or are you talking thrust moment arm, and I am applying it to thrust >vector angles? Or did I miss something? (Always likely...) Advice welcome - > >Thanks >Richard Pike >MKIII N420P (420ldPoops) > >At 12:16 AM 12/10/2005, you wrote: > > > > > >The pitching moment due to thrust is the thrust times > >the moment arm to the cg, not the Aero center. (Drag adds its moment as > >drag times its moment arm to the cg but it doesn't change with thrust > >setting, only with speed.) To change the thrust moment arm significantly > >would require so much angle to get the effect you want that it would be > >terrible for prop efficiency ( not to mention result in yaw due to the > >higher aoa and velocity on the prop on one side of the plane versus the > >other, p-factor in cruise is a very bad thing). The engine is fairly close > >to the CG front to back so you would have to tilt the engine many degrees >to > >reduce the thrust line moment arm significantly. If the engine was farther > >back then only a bit of angle change would reduce the thrust moment arm >much > >more. If you raise the engine too much the plane will not have enough >pitch > >control to overcome the pitch due to thrust and you will not be able to > >rotate or climb. > > > > > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Thrust line change
Date: Dec 10, 2005
| Once this is properly | determined, then we determine if the prop is vertical. Then we go from there. | | Richard Pike Richard/Gang: Another factor you must determine is how much the pitch attitude the engine is going to change from dead engine on the ground to cruise power in the air. The Lord Mounts will allow the engine to push down some in the front and up some in the rear. Will also cock the engine a little as the result of torque. I never realized how much until I was observing the 447 on my Firestar, tied down and increasing and decreasing power. The engine changes attitude from stop to different power settings quite a bit, thus thrust angle. I've started playing around with this way back in FS days. For the MKIII with 912ULS, I raise the front of the engine 5/8". This puts the angle of the prop 90 deg to the bottom of the wing when the engine is off. Just guessing, but I figure the rear of the engine is going to come up a bit and the front down just a tad under cruise power, or about right to give me a thrust line that is parallel to relative wind. I check this with my old eye ball by looking at the wing tip in relation to the horizon in straight and level flight at cruise power. Is it exact? I doubt it, but I think it is more in line with what I am looking for than leaving the engine level on the engine mounts as designed. A good example of what our Kolbs are doing when we push the throttle forward with an engine at high thrust line is about the same, to me, as pushing a lawn mower in thick grass with small wheels. The harder we push horizontally on the high position of the handle, the more the front wheels of the mower get loaded up and the lighter the rear wheels, to the point of them coming right off the lawn and tipping up the rear. I believe that is exactly what we are experiencing with our Kolbs. Do I have numbers, diagrams, bell curves, slide rules, and backing by Kolb Aircraft? Nope. Just a lot of hours flying, tinkering, experimenting, and playing with my Kolbs. john h MKIII/912ULS hauck's holler, alabama ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Thrust line change
Date: Dec 10, 2005
| What would you say the angle of the bottom of your wing is relative | to the horizon while in straight and level flight? | | Richard Pike Richard P/Gang: Heck, what ever is the normal angle of attack at 85mph straight and level. 3 or 4 degs?? About the same angle as a B-52 approach. ;-) john h ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 11, 2005
The main difference with the 582 in terms of jetting is due to the rotary intake valve instead of the piston-skirt induction of the aircooled motors - this causes one of the cylinders to run slightly leaner than the other one. On the 618, which also used the rotary valve, the difference was enough that the carbs actually had to be jetted differently. On the 582, though, the difference isn't enough to require different jets in each carb, but the technique is to jet both a bit rich overall so the lean cylinder runs rich enough. So, unlike on the aircooled motors, you've got a bit narrower of a range of mixture to play with before you're too lean on the one cylinder or too rich on the other. This makes it a bit harder to get the jetting just right. But the rotax recommended jetting for your altitude and temp gets you pretty close.... LS N646F >All > >A couple of weeks ago when the weather got cold here in Virginia I had >trouble getting a satisfactory mag check. The manual states to run up to >3500 rpm and check each mag for no more than 300 rpm drop. During the hot >summer months I was able to get good mag check with my needle set in the >lowest position on my 582 blue head. When the temperature dropped into the >upper thirties/lower forties I could not get my engine to turn more than >3000 rpm before it would bog down. I used the choke and it would turn up >to 4000 rpm. Armed with that information I called Lockwood Aviation and >they advised me to raise the needle in the carbs. I put my clip in the >third notch from the top and it runs great. > >This is the first water cooled 2 stroke rotax I have owned and I am finding >it somewhat different to tune than my prior 277/377/447 air cooled engines. > I have also found out in the cold weather that I needed to install about >4 " of aluminum sheeting on the face of each radiator to keep the water >temperature at least 150 degrees. This morning the OAT was 32 and I was >able to keep my water temp at 152 with 5800 rpm. > >Since I have an electrical system on the MK III X and I had an electric >vest left over from my motorcycling days, I took John Hauck's advise and >hooked up the vest to the battery. What a great easy way to stay warm >without all the hassles of installing a heater system. With the thermostat >on 0/1 position I was warm and my voltage meter indicated a 13.2 volts so >the vest did not take prevent the battery from being charged while I was >flying. Thanks John. > >Jim Ballenger >MK III X 582 >Virginia Beach, VA > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 11, 2005
| The main difference with the 582 in terms of jetting is due to the rotary | intake valve instead of the piston-skirt induction of the aircooled motors - | | LS Morning LS/Gang: Could you explain "piston-skirt indiction" please. Thanks, john h ________________________________________________________________________________
From: "Jim Ballenger" <ulpilot(at)cavtel.net>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 11, 2005
LS Thanks for the info. Jim ----- Original Message ----- From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com> Subject: RE: Kolb-List: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC VEST TESTI > > > The main difference with the 582 in terms of jetting is due to the rotary > intake valve instead of the piston-skirt induction of the aircooled > motors - > this causes one of the cylinders to run slightly leaner than the other > one. > On the 618, which also used the rotary valve, the difference was enough > that > the carbs actually had to be jetted differently. > > On the 582, though, the difference isn't enough to require different jets > in > each carb, but the technique is to jet both a bit rich overall so the lean > cylinder runs rich enough. So, unlike on the aircooled motors, you've got > a > bit narrower of a range of mixture to play with before you're too lean on > the one cylinder or too rich on the other. This makes it a bit harder to > get > the jetting just right. But the rotax recommended jetting for your > altitude > and temp gets you pretty close.... > > LS > N646F > > >>All >> >>A couple of weeks ago when the weather got cold here in Virginia I had >>trouble getting a satisfactory mag check. The manual states to run up to >>3500 rpm and check each mag for no more than 300 rpm drop. During the hot >>summer months I was able to get good mag check with my needle set in the >>lowest position on my 582 blue head. When the temperature dropped into >>the >>upper thirties/lower forties I could not get my engine to turn more than >>3000 rpm before it would bog down. I used the choke and it would turn up >>to 4000 rpm. Armed with that information I called Lockwood Aviation and >>they advised me to raise the needle in the carbs. I put my clip in the >>third notch from the top and it runs great. >> >>This is the first water cooled 2 stroke rotax I have owned and I am >>finding >>it somewhat different to tune than my prior 277/377/447 air cooled >>engines. >> I have also found out in the cold weather that I needed to install about >>4 " of aluminum sheeting on the face of each radiator to keep the water >>temperature at least 150 degrees. This morning the OAT was 32 and I was >>able to keep my water temp at 152 with 5800 rpm. >> >>Since I have an electrical system on the MK III X and I had an electric >>vest left over from my motorcycling days, I took John Hauck's advise and >>hooked up the vest to the battery. What a great easy way to stay warm >>without all the hassles of installing a heater system. With the >>thermostat >>on 0/1 position I was warm and my voltage meter indicated a 13.2 volts so >>the vest did not take prevent the battery from being charged while I was >>flying. Thanks John. >> >>Jim Ballenger >>MK III X 582 >>Virginia Beach, VA >> >> > > > ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 12, 2005
Hey all, This is where the skirt of the piston acts as the intake valve. On the aircooled rotaxen, the intake ports are lower in the sleeve (and on the other side) than the exhaust ports. As the piston goes up, the skirt clears the port, causing an opening into the crankcase - the vacuum from the upgoing piston pulls the air/fuel mixture in in the familiar way. On the power stroke, the skirt blocks the port off closing it, allowing crankcase pressure to build up for the exhaust stroke.... The 582 uses a mechanically driven rotary valve to control the intake, which involves some extra machinery and complexity. The advantage of the rotary valve, though, is very smooth running and broad powerband. Sure enough, the 582 runs like a swiss watch... The piston skirt induction motors are much simpler, but they tend to be peakier and behave more "2-strokey".... I still far prefer the simplicity of piston skirt induction....... There are other induction methods for 2-strokes besides these, such as reed valves and crankshaft induction (these are common on R/C 2-stroke motors)... LS N646F >Morning LS/Gang: > >Could you explain "piston-skirt indiction" please. > >Thanks, > >john h > > ________________________________________________________________________________
Date: Dec 11, 2005
From: "David L. Bigelow" <dlbigelow(at)verizon.net>
Subject: RE: Thrust Line
The pitching moment due to thrust is dependent on the distance the thrust line is from the center of drag - not the CG. If the thrust line is right through the center of drag, there will be no pitch moment up or down. Can't show it here, but a vector diagram of an aircraft in equilibrium will illustrate this fact. The center of drag of a high wing aircraft like a Kolb is somewhere below and behind the center of lift of the wing. Because of the tail boom, you cannot get the thrust line low enough on a Kolb to avoid a nose down pitching moment when thrust is applied. Changing the thrust vector direction by tilting the engine up or down will affect the equation somewhat, but not enough to compensate for the loss of efficiency. Best angle of the thrust line is about 6 degrees down from the chord of the wing. This allows the aircraft to have all the thrust vector pointed parallel to the airflow at a normal flying angle of attack of the aircraft, which is the most efficient. Dave Bigelow Kamuela, Hawaii FS2, DCDI 503 ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: looking for 912
Date: Dec 12, 2005
Hi all, Speaking of 912's... I'm starting to put feelers out for a low to mid-time 912 in good shape. The kolbra is looking like the #1 contender for my next plane, so I'm looking for a 912 to power it. A new one is a little out of reach at the moment, so a good used motor is what I'm looking for right now. If anyone knows of a good deal, let me know.... Thanks, LS N646F ________________________________________________________________________________
Subject: monument valley
From: Erich_Weaver(at)URSCorp.com
Date: Dec 12, 2005
12/12/2005 01:09:15 PM Hey gang I havent been paying close attention lately, so not sure if the word has gotten out, but I recently sold my Mrk III and trailer to Robert Laird. I have been working on an RV-7A project for the past year, and decided that sooner or later I was going to have to give up my first love. Still a bit sad about it, but will soon be receiving the engine for the RV, and am getting very excited about that. For all those who havent been, Monument Valley is a fantastic place to fly, and Im proud to count myself as one of the original founders of what now appears to be an annual tradition. Because of me, we all now know that fly-bys of the restaurant balcony are frowned on by management! I hope to see you all there in May 2006, but its going to be a bit to soon to take the RV, so I'll be ground bound. I believe Robert is excited about MV as well, so I expect you will be seeing him there in the future with a familiar looking plane, although Im not sure about his 2006 plans Best regards to all my Kolb friends Erich Weaver ________________________________________________________________________________
Date: Dec 12, 2005
From: Robert Laird <rlaird(at)cavediver.com>
Subject: Re: monument valley
I'd like to thank Erich for his offering up his "baby" to me, and very glad to finally own a Kolb. I took it for a romp around the pattern on Saturday and, compared to what I was flying before, the Kolb is nimble and quick... a real joy to fly. As for Monument Valley, it's my _plan_ to be there, but there are two problems: one is, my son will still be in school that weekend, so if I make it, it would have to be solo; and, two, I've just started a new job and it's still up in the air (no pun intended) whether I'll be able to get the time off for that period. But, if the gods favor idiots and fools, then I'll be there for certain! -- Robert On 12/12/05, Erich_Weaver(at)urscorp.com wrote: > > Hey gang > > I havent been paying close attention lately, so not sure if the word has > gotten out, but I recently sold my Mrk III and trailer to Robert Laird. I > have been working on an RV-7A project for the past year, and decided that > sooner or later I was going to have to give up my first love. Still a bit > sad about it, but will soon be receiving the engine for the RV, and am > getting very excited about that. > > For all those who havent been, Monument Valley is a fantastic place to > fly, and Im proud to count myself as one of the original founders of what > now appears to be an annual tradition. Because of me, we all now know that > fly-bys of the restaurant balcony are frowned on by management! I hope to > see you all there in May 2006, but its going to be a bit to soon to take > the RV, so I'll be ground bound. I believe Robert is excited about MV as > well, so I expect you will be seeing him there in the future with a > familiar looking plane, although Im not sure about his 2006 plans > > Best regards to all my Kolb friends > > Erich Weaver > > ________________________________________________________________________________
From: "Jim Ballenger" <ulpilot(at)cavtel.net>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 12, 2005
LS Very informative. Thanks for the insight and explanation of the piston skirt/rotary valve issue. It kinda makes ense to me. Jim ----- Original Message ----- From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com> Subject: Re: Kolb-List: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC VEST TESTI > > > Hey all, > > This is where the skirt of the piston acts as the intake valve. On the > aircooled rotaxen, the intake ports are lower in the sleeve (and on the > other side) than the exhaust ports. As the piston goes up, the skirt > clears > the port, causing an opening into the crankcase - the vacuum from the > upgoing piston pulls the air/fuel mixture in in the familiar way. On the > power stroke, the skirt blocks the port off closing it, allowing crankcase > pressure to build up for the exhaust stroke.... > > The 582 uses a mechanically driven rotary valve to control the intake, > which > involves some extra machinery and complexity. > > The advantage of the rotary valve, though, is very smooth running and > broad > powerband. Sure enough, the 582 runs like a swiss watch... The piston > skirt > induction motors are much simpler, but they tend to be peakier and behave > more "2-strokey".... > > I still far prefer the simplicity of piston skirt induction....... > > There are other induction methods for 2-strokes besides these, such as > reed > valves and crankshaft induction (these are common on R/C 2-stroke > motors)... > > LS > N646F >>Morning LS/Gang: >> >>Could you explain "piston-skirt indiction" please. >> >>Thanks, >> >>john h >> >> > > > ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 12, 2005
| piston skirt/rotary valve issue. | Jim | Jim B/LS/Gang: Correct me if I am wrong, please. Isn't this system more commonly called a "piston/port" system? The system used on the 503 and others, other than the 582? john h MKIII ________________________________________________________________________________
From: "lucien stavenhagen" <lstavenhagen(at)hotmail.com>
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT/RADIATOR TIPS/ELECTRIC
VEST TESTI
Date: Dec 12, 2005
>Jim B/LS/Gang: > >Correct me if I am wrong, please. Isn't this system more commonly >called a "piston/port" system? The system used on the 503 and others, >other than the 582? Nope, you're not wrong, I've heard piston ported as well...... LS N646F >john h >MKIII > > ________________________________________________________________________________
From: "Michael Bigelow" <orcabonita(at)hotmail.com>
Subject: Re: RE: Thrust Line
Date: Dec 12, 2005
As I am building a Kolb I have been watching the thread about pitch down with power with great interest. Changing the thrust line angle works very well on a standard airplane where the engine is mounted in the nose, and also works well on a Jet airplane where the engines are mounted on the tail. This is because in these two cases the engine is far enough foward or behind the CG, that the angle of the thrust has an effect of pitching the airplane either up or down. For example, with the engine in the nose, down thrust will pull the nose downward, and pitch the plane down. An engine in the tail with downthrust will push the tail of the airplane up cuasing the plane to pitch down. In the Kolb, the prop is very close to the CG of the airplane as far as pitch goes. Pointing the prop up (higher thrust angle) and having the engine push down right near the CG will have no noticable effect on pitch. Bottom line is, if you want to help pitch the airplane by using thrust angle, it needs to be done much further foward or further aft of the PITCH CG. Its just not going to happen on a Kolb. With the engine and prop mounted far above the center of drag, the kolb will always pitch down with power, there is just no getting around it. Best thing is to lower the engine and prop as much as possible, without striking the boom. Michael Bigelow ________________________________________________________________________________
From: "Jim Baker" <jlbaker(at)telepath.com>
Date: Dec 12, 2005
Subject: Re: ROTAX 582 JET NEEDLE ADJUSTMENT
> Thanks for the insight and explanation of the > piston skirt/rotary valve issue. It kinda makes ense to me. For anyone really serious about understanding the two stroke engine..... http://kawtriple.com/mraxl/jennings.htm I've got a hard copy of the book referenced by the link above. Wouldn't part wth it for love nor money (out of print and signed by Jennings). Jim Baker 580.788.2779 '71 SV, 492TC Elmore City, OK ________________________________________________________________________________
Date: Dec 12, 2005
From: Ron Hoyt <rrhoyt(at)ieee.org>
Subject: Re: Thrust line change
I have been reading the thread with great interest since my mark III requires a large rudder tab that I dislike. I have been mulling over the impact of rotating the 912 a couple of degrees in azimuth to mitigate the yaw that the rudder tab corrects. I tried flexing the vertical stabilizer to effect a change but it was not noticeable in flight. Christopher's line of reasoning implies that the moment arm is small and a substantive change is not likely. Is there any experience out there with this trimming. Ron Kolb Mark III C N232S ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Thrust line change
Date: Dec 12, 2005
| Is there any | experience out there with this trimming. | | Ron Ron H/Gang: Yes, a little. I have been dabbling with Kolbs for 21 years, and my MKIII for the last 15 years. Did the engine rotation thing, left and right, up and down, on my FS, back in the mid 80's. Did the same thing on the MKIII with the engine. Tried different settings for the leading edge of the upper vertical stabilizer, offset as much as 1 3/8" to the left, with little positive effect. Wasn't worth the effort. Put it back where it belonged in the center. During construction I knew I was going to have to do something about the pitch down caused by power, and the tendancy to roll left when flying left seat solo. To solve those problems I fly right seat and made up some adjustable horizontal stabilizer forward mounts. Experiemented lowering at different levels until I found the sweet spot for the airplane and me. TNK now has these mounts available, I have been told. Adverse yaw is caused by the way the prop wash hits the tail section. I flew for nearly a 1,000 hours 1/2 ball out of trim with a small trim tab, one rudder rib bay width long. Now I have one twice as long and I fly trimmed in pitch. No noticeable difference in performance between then and now. The old MKIII is happy flying in or out of yaw trim. Now I don't have to push a lot of right pedal to swing it back into trim. BTW, a lot of folks on the Kolb List refer to the "slip/skid" indicator as a turn and bank indicator. Don't think so. It does three things. Tells me when I am skidding, slipping, and when I am in trim. If I want to check its accuracy, I can stick a yaw string on the lower center of the windshield or top of the nose cone to see if they agree. Nothing wrong with the big trim tab or a lot of forced trim to take the forward stick pressure off your hand and arm. This is the nature of the MKIII. Most of the things folks are experiementing with now, trying to improve on Kolbs, has already been done. With the exception of seriously cleaning up aerodynamically a couple areas of my old MKIII, she is going to stay as she is. With nearly 2,500 hours flying her from the right seat (all those hours on her are mine), I pretty much accept the way she is. I'm happy with her. That is why I still fly her. Not really concerned too much on why she does what she does. All I know is she does a good job for me. It is still fun trying to improve your own airplane, expecially is it is new without a whole bunch of years and hours on it. I know. I have been there. It was a lot of fun, frustrating at times, but I'd probably do it again if I could. Take care, john h MKIII, 912ULS hauck's holler, alabama ________________________________________________________________________________
Date: Dec 13, 2005
From: Ted Cowan <trc1917(at)direcway.com>
Subject: thrust line
Okay, gotta put my two cents in here too. I am not a tech head like some of you guys with your rulers and scales. I do know something about the Kolb Sling Shot when it comes to the engine alignment. If you mount the 582 on the SS as per the instructions, right on the rubber so to speak, you gotta real horse to ride. I mean, that thing will require so much up elevator to take off and fly you will think your arm is going to break. The obstructions used to recommend raising the rear of the engine off the mounts by some inch or something. Well, my obstructions did not. I learned this from another SS. My engine is mounted on high risers as recommended and supplied by the factory to ensure the wings can be folded. This raising the engine three inches off the saddle really magnified the problem with thrust. After some experimentation of angles, I have the rear of the engine mounted 7/8" higher than the front mounts which makes the rear mounts approx. 3" high and the front mounts 2-1/8" high. I have an extra washer on the left front to help compensate fors torque on takeoff and it makes a world of difference. It may not do much for a long tailed MkIII or FSII but when your boom is short and your wings are barely visible, it makes a world of difference. I must have done something wrong cause this bird flys virtually hands off when the electric/spring elevator trim is set -- which by the way, stays the same for take-off, high speed and low speed. I only change it for the load I am carrying, extra gas, camping equip, etc. I recon my little hick self musta done sometin wrong cause it dont never dive left or behave badly. Oh, ya, by the way, my fuel consumption dropped also by a little. Dont need to be a rocket scientist or college boy to figure out some of this stuff. My opinions. And -- this SHOULD be archived. Ted Cowan, Alabama, SS Driver. Can be seen at our Club web site at: www.homestead.com/southernflyers ________________________________________________________________________________
From: "c b" <seedeebee(at)hotmail.com>
Subject: Re: Monument Valley 2006
Date: Dec 13, 2005
All, I plan to attend. Is anyone flying there from California? Chris Banys Mk III 912UL N10FR ________________________________________________________________________________
From: "c b" <seedeebee(at)hotmail.com>
Subject: Flat v. Conical Air Filters for the 912
Date: Dec 13, 2005
Hey all, Anyone have any experience with both the flat & conical K&N air filters on the 912? I have the flat ones right now, they basically present a pie plate to the wind and make the air do a 2 90 degree bends before entering the carbs. The conical ones should allow for more ram air effect. But I wanted to check with you all before I spent the $75. Happy Flying, Chris Banys Mk III 912UL N10FR ________________________________________________________________________________
From: FlyColt45(at)aol.com
Date: Dec 13, 2005
Subject: Re: Inspection Repairman Cert
All, I also took the Repairman LSA Insp Rating Course here in Lantana, FL last week. Since mine is an amateur built - experimental and I'll will get the repairman's certificate for my plane, I really didn't need this course but wanted to know as much as possible about the inspection side of things. In that regard the course was great for me - since I knew little about good and bad welds, good and bad wood and even found out why Aero thane is much better than auto paint with clear coat. The discourse with the instructors, (Jerry Stradtmiller and Lisa Turner), between and after classes were "gold". I even passed the test! If you are going the LSA route for your Kolb - its a great course to take. Now - on to the Rotax 912 course : ) Jim PA/FL ________________________________________________________________________________
From: "Larry Bourne" <biglar(at)gogittum.com>
Subject: Re: Monument Valley 2006
Date: Dec 13, 2005
Not so far.......I'll be driving from Palm Springs. Do not Archive. Larry Bourne Palm Springs, CA Building Kolb Mk III N78LB Vamoose www.gogittum.com ----- Original Message ----- From: "c b" <seedeebee(at)hotmail.com> Subject: Kolb-List: Re: Monument Valley 2006 > > All, > > I plan to attend. Is anyone flying there from California? > > Chris Banys > Mk III 912UL > N10FR > > > ________________________________________________________________________________
Date: Dec 13, 2005
From: "Jack B. Hart" <jbhart(at)onlyinternet.net>
Subject: Re: Thrust line change & Yaw Correction
>Date: Mon, 12 Dec 2005 21:03:11 -0600 >To: kolb-list(at)matronics.com >From: Ron Hoyt <rrhoyt(at)ieee.org> >Subject: Kolb-List: Re: Thrust line change >Sender: owner-kolb-list-server(at)matronics.com >Reply-To: kolb-list(at)matronics.com >X-Virus-Scanned: by amavisd-new at onlyinternet.net > > >I have been reading the thread with great interest since my mark III >requires a large rudder tab that I dislike. I have been mulling over >the impact of rotating the 912 a couple of degrees in azimuth to >mitigate the yaw that the rudder tab corrects. I tried flexing the >vertical stabilizer to effect a change but it was not noticeable in >flight. Christopher's line of reasoning implies that the moment arm >is small and a substantive change is not likely. Is there any >experience out there with this trimming. > Ron, & Kolbers, I do not know if this is possible with the Mark III, but I rotated my reduction drive assembly off to one side to correct for yaw on my FireFly. This gives an increased moment arm that Chris A. talks about. One other thing, that I have discovered (more like stumbled on) with the FireFly. When I was taking the play out of the aileron control system, I discovered part of the problem was caused by the saddle arrangement that comes down from the bolt through the main tube that exits at the rear of the fuselage. The holes drilled through the saddle arms are too large. This lets the saddle rock from side to side as the stick is displaced from side to side. The only way I could think of to solve this problem was to re drill and ream the holes through the saddle ends and insert bronze flange oil-lite bearings so that the play could be removed. Then I thought, the holes through the fuselage through which the main bolt pass are also oversized. With a loose through bolt, a long tail tube and the tail assembly, their relationship to the wing can change during flight. The saddle arms must rotate on this through bolt, so if one completely tightens the nut the flaperons become fixed. As an experiment, I tightened the nut and went on a test flight. Just by tightening the nut the ball moved a half a diameter toward the center. This indicates a small change up by the fuselage can make a fairly large change in yaw. This is reasonable when one thinks about the relative distances from the cg. It may be useful to place a shim washer or two in between the tube and the inside of the fuselage to shift the position of the tail relative to the wing, etc. Seems low risk, inexpensive, and a fairly simple experiment to do. I purchased some flanged oil-lite bronze bushings to put over the bolt so that I could tightened the through bolt nut completely. But moving has gotten in the way. The bushings are lost in a box and will remain lost until, I can get my shop put together. Jack B. Hart FF004 Winchester, IN ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Flat v. Conical Air Filters for the 912
Date: Dec 13, 2005
| The conical ones should allow for more ram air effect. | | Chris Banys Hi Chris/Gang: The 912 engine was designed as a tractor, rather than a pusher engine. Thus the carbs are actually on the wrong end of the engine for the pusher configuration. Check out an old BMW twin motorcycle. The Bing carb was designed to operate 180 deg from the way we use them on our pushers. The Bing gets its info to adjust the piston and fuel needle up and down from two static pressure sources: 1- One is the float bowl vent tube 2- The other is a port on the lip of the carb In order to do its job correctly, the two static sources need to be reading off the same sheet of music. On the flat air filters there is a plug that can be popped our so you can insert the float bowl vent tube into the air filter. This will have both ports reading same static pressure. Ram air into conical filters is not good, in my opinion. I use some conical fiber glass covers on my conical filters with the flat chamber vent tube inserted into the cover. Works good for me and I do not get the ram air effect to upset the Bing's mind. I had a problem with fuel vapor standoff being blown out of the flat filter on the right side. This kept the right carb a nice brown color from the auto fuel. The covers on the conical filters correct this. The problem is not the same on all installations on Kolbs. It is a matter of how the air flows over the engine. My system was aggrevated by its particular air flow. john h MKIII/912ULS hauck's holler, alabama ________________________________________________________________________________
From: "flykolb" <flykolb(at)wowway.com>
Subject: Rotax 670
Date: Dec 14, 2005
2.32 DATE_IN_FUTURE_12_24 Date: is 12 to 24 hours after Received: date Kolbers, Does anyone on the list have experience with a rotax 670 on a Mark III? Jim Mark III Michigan ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: tail boom/flaperon link bolt bushings/prop wash and other
stuff
Date: Dec 13, 2005
| Certainly getting the tail aligned straight | both side to side and vertical twist wise is probably one of the most | important parts to trimming up a Kolb. | | Topher Hi Topher/Gang: Surely you know me well enough now to know I know diddily squat about formulas, graphs, charts, etc. However, have done a little flying over the years in our little Kolbs. No matter how well be build our little airplanes, how well we insure they are as true and correct as possible, we are going to have a couple inherent problems, especially with the MKIII. I believe it has to do with the way the prop wash hits one side of the tail section. Don't even have to see this to understand it. One can feel it. Stand behind a MKIII with the engine running. On one side of the vertical stabilizer it will blow you down. On the other, very little prop blast. To back this up, on long flights especially, the left side of the vertical stab and rudder will have oil and fuel residue spatters coming from the oil tank vent. Also the top of the left horizontal stabilizer. I believe when prop wash is not hitting the tail section uniformly, we are going to have yaw, primarily, and maybe some pitch problems. Not talking about all aircraft, only my MKIII. Thus, the large rudder trim tab to center the trim ball. john h MKIII/912ULS hauck's holler, alabama ________________________________________________________________________________
From: "chris davis" <scrounge69(at)comcast.net>
Subject: NORMS MK3 CRASH
Date: Nov 13, 2005
HI LIsters its been a year and a month since I was the passenger with Norm at the Kolb factory. Rest his soul, I was in the hospital til July 15 2005. I had a tour of the factory in the morn then donnys ears perked up and hr said" here comes our demo pilot" I had just bought a beautiful MK3From Bob Broucis, the day before and sold my firestar KXP two weeks before after 10 years of flying and dreams of the FAA light sport aircraft filling my mind and my heart. I had an excellent year commercial fishing and had been searching for a flyin community for 10 years. I found one and bought a 4 acre site and a new singlewide big enough for my my 85 year old ex pilot Dad and my step mom my wife and myself in O'Brien Florida thats on the Suwannee river in NW Florida , So taking a demo flight in the factories two place seem like a good idea , my last flight in a MK3 was in the late 80s at Sun and Fun with JOHN HAUCK well this decision was the last thing I remember until Jan 5, 2005. I dont remember Norm or the walkaround he did or the check ride and another walkaround that he and I did but my wife does !she was on the ground taking pictures and hoping for a great uneventful flight .I don't remember the fact that we did a touch and go and on the next flight my wife says " she heard and saw us take off and then we went behind the hanger and she thought " we left the area because she couldn't hear the Rotax" but is smart enough to know it was a quiet 4stroke Rotax not like my 503 but the she saw us come around the hanger with the engine out and crash into the end of the runway she was there right after Donny and he said "there both alive " as he ran to the phone , My wife Becky is an R.N.and ran to the planeopen the door and I sat up saying " my back" Norm wasn't moving , she gave him mouth to mouth and he turned from blue to pink as the EMTs arrived got me out and said" he is gone" about Norm. What a great bunch of rescue people they have in London Kentucky, They put me in a helicopter and had me at University of Kentucky Hospital in a matter of minutes I was busted up pretty bad . Six broken ribs broken sternum a crushed ,80% spine my pelvis was broken into 9 pieces .which are now bolted together with 2 seven inch stainless lag bolts I've got two 3\8 stainless rods going down my spine and there is a spot above my tailbone that the two ss rods are boxed together to freeze the place where my spinal cord was crushed I say was because I am learning to walk, I can lift my body which weighed 148 lbs when I got out of the Hosp after 9months ,but now weighs alittle over 190ibs most of it is muscle University of Kentucky Hosp. is a wondrous place , They did a great job on me and they let my wife live in there waiting room for two weeks ,because she didn't want to be away from me ,I was in such bad shape .She is quite a woman 91\2 months in the hosp. she was by my side every day accept one there was 8ft of snow in the driveway caused her to miss a day!The reason am writing is That I had some really excellent lawyers that my wife Hired when they thought I was going to be a quadriplegic or worse they considered suing everyone ,ROTA,KOLB , THE PILOT I said no to them all Rota? we all know the 4 strokes run and the NTSB took the engine to Florida hooked it up to pure fuel and ran it for hours ran like a dream ,KOLB we all know that Kolb's are so well designed that if I had been in another ultrslight type aircraft we would both probly be dead ,crome moly cockpit and all , the PILOT I didn't want to hurt his family , then the insurance company that held the Liability policy that Norm had paid for for years told my lawyers there would be no argument .he paid for it and they would pay me ! no harm to his wife or kids and I am going to make a deposit in the Labhart children's fund after all in htis KOLB family we are all -- brothers& sisters are we not ? one more thing I would like to say the reason I think you all know why I didn't sue KOLB is I still want to build a MKIII and I believe I will . first I need to build a shop and hanger in O'Brien the get a kit and work my way through it . in 3or4or5 years maybe I will fly , MY wife says she won't stop me , WHAT A WIFE she is the reason I live . Thanks for all the good will you all wished us back in November Norm was lucky to have you all for friends . Sorry about the long story vie haven't had a computer fo a while . it would be great to hear from any of you any time . a KOLBER forever Chris davis cape cod ma.& O'Brien Fl. ________________________________________________________________________________
From: "Ed Chmielewski" <edchmiel(at)mindspring.com>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
Chris, Good to see you're on the road to recovery. "I said no to them all (snip) I am going to make a deposit in the Labhart children's fund" You, sir, are a class act. The best to you and your wife and family!! Ed in JXN MkII/503 ----- Original Message ----- From: "chris davis" <scrounge69(at)comcast.net> Subject: Kolb-List: NORMS MK3 CRASH > > HI LIsters its been a year and a month since I was the passenger with > Norm at > the Kolb factory. ________________________________________________________________________________
From: "Silver Fern Microlights Ltd" <kiwimick(at)sfmicro.fsnet.co.uk>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
Hey Chris, Great you are doing well. Good to read your story, shame there is not more people around like you, seems like sueing has become a world sport nowdays. I too am lucky to have an understanding wife, I was lucky to survive a serious paragliding accident but she supports me in everything I do. I know what the risks are everytime I leave the ground. I hope you achieve your ambition of building your new Kolb, I have flown dozens of types, and I am a microlight instructor and the Kolb still puts a smile on my face everytime I fly it. All the best brother Kolber Kind Regards Mike Moulai UK/European Kolb Distributor ----- Original Message ----- From: "chris davis" <scrounge69(at)comcast.net> Subject: *** SPAM *** Kolb-List: NORMS MK3 CRASH > > HI LIsters its been a year and a month since I was the passenger with > Norm at > the Kolb factory. Rest his soul, I was in the hospital til July 15 2005. > I had > a tour of the factory in the morn then donnys ears perked up and hr said" > here > comes our demo pilot" I had just bought a beautiful MK3From Bob Broucis, > the > day before and sold my firestar KXP two weeks before after 10 years of > flying > and dreams of the FAA light sport aircraft filling my mind and my heart. > I had > an excellent year commercial fishing and had been searching for a flyin > community for 10 years. I found one and bought a 4 acre site and a new > singlewide big enough for my my 85 year old ex pilot Dad and my step mom > my wife > and myself in O'Brien Florida thats on the Suwannee river in NW Florida , > So > taking a demo flight in the factories two place seem like a good idea , my > last > flight in a MK3 was in the late 80s at Sun and Fun with JOHN HAUCK well > this > decision was the last thing I remember until Jan 5, 2005. I dont remember > Norm > or the walkaround he did or the check ride and another walkaround that he > and I > did but my wife does !she was on the ground taking pictures and hoping for > a > great uneventful flight .I don't remember the fact that we did a touch > and go > and on the next flight my wife says " she heard and saw us take off and > then we > went behind the hanger and she thought " we left the area because she > couldn't > hear the Rotax" but is smart enough to know it was a quiet 4stroke Rotax > not > like my 503 but the she saw us come around the hanger with the engine out > and > crash into the end of the runway she was there right after Donny and he > said > "there both alive " as he ran to the phone , My wife Becky is an R.N.and > ran to > the planeopen the door and I sat up saying " my back" Norm wasn't > moving , > she gave him mouth to mouth and he turned from blue to pink as the EMTs > arrived > got me out and said" he is gone" about Norm. What a great bunch of rescue > people they have in London Kentucky, They put me in a helicopter and had > me at > University of Kentucky Hospital in a matter of minutes I was busted up > pretty > bad . Six broken ribs broken sternum a crushed ,80% spine my pelvis was > broken > into 9 pieces .which are now bolted together with 2 seven inch > stainless lag > bolts I've got two 3\8 stainless rods going down my spine and there is a > spot > above my tailbone that the two ss rods are boxed together to freeze the > place > where my spinal cord was crushed I say was because I am learning to walk, > I can > lift my body which weighed 148 lbs when I got out of the Hosp after > 9months ,but > now weighs alittle over 190ibs most of it is muscle University of Kentucky > Hosp. is a wondrous place , They did a great job on me and they let my > wife live > in there waiting room for two weeks ,because she didn't want to be away > from me > ,I was in such bad shape .She is quite a woman 91\2 months in the hosp. > she was > by my side every day accept one there was 8ft of snow in the driveway > caused her > to miss a day!The reason am writing is That I had some really excellent > lawyers > that my wife Hired when they thought I was going to be a quadriplegic or > worse > they considered suing everyone ,ROTA,KOLB , THE PILOT I said no to > them all > Rota? we all know the 4 strokes run and the NTSB took the engine to > Florida > hooked it up to pure fuel and ran it for hours ran like a dream ,KOLB we > all > know that Kolb's are so well designed that if I had been in another > ultrslight > type aircraft we would both probly be dead ,crome moly cockpit and all , > the > PILOT I didn't want to hurt his family , then the insurance company that > held > the Liability policy that Norm had paid for for years told my lawyers > there > would be no argument .he paid for it and they would pay me ! no harm to > his wife > or kids and I am going to make a deposit in the Labhart children's fund > after > all in htis KOLB family we are all -- brothers& sisters are we not ? one > more > thing I would like to say the reason I think you all know why I didn't > sue KOLB > is I still want to build a MKIII and I believe I will . first I need to > build > a shop and hanger in O'Brien the get a kit and work my way through it . in > 3or4or5 years maybe I will fly , MY wife says she won't stop me , WHAT A > WIFE > she is the reason I live . Thanks for all the good will you all wished > us back > in November Norm was lucky to have you all for friends . Sorry about the > long > story vie haven't had a computer fo a while . it would be great to hear > from > any of you any time . a KOLBER forever Chris davis cape cod ma.& O'Brien > Fl. > > > ________________________________________________________________________________
From: russ kinne <kinnepix(at)earthlink.net>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
I for one have seldom met, or even heard of, anyone as downright decent, and as fine a person as Chris Davis. The very best of everything to him and his most amazing wife Fair winds to you both Russ Kinne On Nov 13, 2005, at 4:42 PM, chris davis wrote: > > HI LIsters its been a year and a month since I was the passenger with > Norm at > the Kolb factory. Rest his soul, I was in the hospital til July 15 > 2005. I had > a tour of the factory in the morn then donnys ears perked up and hr > said" here > comes our demo pilot" I had just bought a beautiful MK3From Bob > Broucis, the > day before and sold my firestar KXP two weeks before after 10 years of > flying > and dreams of the FAA light sport aircraft filling my mind and my > heart. I had > an excellent year commercial fishing and had been searching for a > flyin > community for 10 years. I found one and bought a 4 acre site and a new > singlewide big enough for my my 85 year old ex pilot Dad and my step > mom my wife > and myself in O'Brien Florida thats on the Suwannee river in NW > Florida , So > taking a demo flight in the factories two place seem like a good idea > , my last > flight in a MK3 was in the late 80s at Sun and Fun with JOHN HAUCK > well this > decision was the last thing I remember until Jan 5, 2005. I dont > remember Norm > or the walkaround he did or the check ride and another walkaround that > he and I > did but my wife does !she was on the ground taking pictures and hoping > for a > great uneventful flight .I don't remember the fact that we did a > touch and go > and on the next flight my wife says " she heard and saw us take off > and then we > went behind the hanger and she thought " we left the area because she > couldn't > hear the Rotax" but is smart enough to know it was a quiet 4stroke > Rotax not > like my 503 but the she saw us come around the hanger with the engine > out and > crash into the end of the runway she was there right after Donny and > he said > "there both alive " as he ran to the phone , My wife Becky is an > R.N.and ran to > the planeopen the door and I sat up saying " my back" Norm wasn't > moving , > she gave him mouth to mouth and he turned from blue to pink as the > EMTs arrived > got me out and said" he is gone" about Norm. What a great bunch of > rescue > people they have in London Kentucky, They put me in a helicopter and > had me at > University of Kentucky Hospital in a matter of minutes I was busted > up pretty > bad . Six broken ribs broken sternum a crushed ,80% spine my pelvis > was broken > into 9 pieces .which are now bolted together with 2 seven inch > stainless lag > bolts I've got two 3\8 stainless rods going down my spine and there > is a spot > above my tailbone that the two ss rods are boxed together to freeze > the place > where my spinal cord was crushed I say was because I am learning to > walk, I can > lift my body which weighed 148 lbs when I got out of the Hosp after > 9months ,but > now weighs alittle over 190ibs most of it is muscle University of > Kentucky > Hosp. is a wondrous place , They did a great job on me and they let my > wife live > in there waiting room for two weeks ,because she didn't want to be > away from me > ,I was in such bad shape .She is quite a woman 91\2 months in the > hosp. she was > by my side every day accept one there was 8ft of snow in the driveway > caused her > to miss a day!The reason am writing is That I had some really > excellent lawyers > that my wife Hired when they thought I was going to be a quadriplegic > or worse > they considered suing everyone ,ROTA,KOLB , THE PILOT I said no to > them all > Rota? we all know the 4 strokes run and the NTSB took the engine to > Florida > hooked it up to pure fuel and ran it for hours ran like a dream ,KOLB > we all > know that Kolb's are so well designed that if I had been in another > ultrslight > type aircraft we would both probly be dead ,crome moly cockpit and all > , the > PILOT I didn't want to hurt his family , then the insurance company > that held > the Liability policy that Norm had paid for for years told my lawyers > there > would be no argument .he paid for it and they would pay me ! no harm > to his wife > or kids and I am going to make a deposit in the Labhart children's > fund after > all in htis KOLB family we are all -- brothers& sisters are we not ? > one more > thing I would like to say the reason I think you all know why I > didn't sue KOLB > is I still want to build a MKIII and I believe I will . first I need > to build > a shop and hanger in O'Brien the get a kit and work my way through it > . in > 3or4or5 years maybe I will fly , MY wife says she won't stop me , WHAT > A WIFE > she is the reason I live . Thanks for all the good will you all > wished us back > in November Norm was lucky to have you all for friends . Sorry about > the long > story vie haven't had a computer fo a while . it would be great to > hear from > any of you any time . a KOLBER forever Chris davis cape cod ma.& > O'Brien Fl. > > ________________________________________________________________________________
From: "Wayne T. McCullough" <blackbird754(at)alltel.net>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
Chris, You do not know me...but to say you are a class act doesn't even come close....I wish you a speedy recovery.....and may God's grace go with with you and your entire family.........Aviators are a special breed of people anyway...... You my friend have always been in our prayers and will continue to do so......maybe I can meet you someday.... Wayne McCullough Kolbra 004 ----- Original Message ----- From: "chris davis" <scrounge69(at)comcast.net> Subject: Kolb-List: NORMS MK3 CRASH > > HI LIsters its been a year and a month since I was the passenger with > Norm at > the Kolb factory. Rest his soul, I was in the hospital til July 15 2005. > I had > a tour of the factory in the morn then donnys ears perked up and hr said" > here > comes our demo pilot" I had just bought a beautiful MK3From Bob Broucis, > the > day before and sold my firestar KXP two weeks before after 10 years of > flying > and dreams of the FAA light sport aircraft filling my mind and my heart. > I had > an excellent year commercial fishing and had been searching for a flyin > community for 10 years. I found one and bought a 4 acre site and a new > singlewide big enough for my my 85 year old ex pilot Dad and my step mom > my wife > and myself in O'Brien Florida thats on the Suwannee river in NW Florida , > So > taking a demo flight in the factories two place seem like a good idea , my > last > flight in a MK3 was in the late 80s at Sun and Fun with JOHN HAUCK well > this > decision was the last thing I remember until Jan 5, 2005. I dont remember > Norm > or the walkaround he did or the check ride and another walkaround that he > and I > did but my wife does !she was on the ground taking pictures and hoping for > a > great uneventful flight .I don't remember the fact that we did a touch > and go > and on the next flight my wife says " she heard and saw us take off and > then we > went behind the hanger and she thought " we left the area because she > couldn't > hear the Rotax" but is smart enough to know it was a quiet 4stroke Rotax > not > like my 503 but the she saw us come around the hanger with the engine out > and > crash into the end of the runway she was there right after Donny and he > said > "there both alive " as he ran to the phone , My wife Becky is an R.N.and > ran to > the planeopen the door and I sat up saying " my back" Norm wasn't > moving , > she gave him mouth to mouth and he turned from blue to pink as the EMTs > arrived > got me out and said" he is gone" about Norm. What a great bunch of rescue > people they have in London Kentucky, They put me in a helicopter and had > me at > University of Kentucky Hospital in a matter of minutes I was busted up > pretty > bad . Six broken ribs broken sternum a crushed ,80% spine my pelvis was > broken > into 9 pieces .which are now bolted together with 2 seven inch > stainless lag > bolts I've got two 3\8 stainless rods going down my spine and there is a > spot > above my tailbone that the two ss rods are boxed together to freeze the > place > where my spinal cord was crushed I say was because I am learning to walk, > I can > lift my body which weighed 148 lbs when I got out of the Hosp after > 9months ,but > now weighs alittle over 190ibs most of it is muscle University of Kentucky > Hosp. is a wondrous place , They did a great job on me and they let my > wife live > in there waiting room for two weeks ,because she didn't want to be away > from me > ,I was in such bad shape .She is quite a woman 91\2 months in the hosp. > she was > by my side every day accept one there was 8ft of snow in the driveway > caused her > to miss a day!The reason am writing is That I had some really excellent > lawyers > that my wife Hired when they thought I was going to be a quadriplegic or > worse > they considered suing everyone ,ROTA,KOLB , THE PILOT I said no to > them all > Rota? we all know the 4 strokes run and the NTSB took the engine to > Florida > hooked it up to pure fuel and ran it for hours ran like a dream ,KOLB we > all > know that Kolb's are so well designed that if I had been in another > ultrslight > type aircraft we would both probly be dead ,crome moly cockpit and all , > the > PILOT I didn't want to hurt his family , then the insurance company that > held > the Liability policy that Norm had paid for for years told my lawyers > there > would be no argument .he paid for it and they would pay me ! no harm to > his wife > or kids and I am going to make a deposit in the Labhart children's fund > after > all in htis KOLB family we are all -- brothers& sisters are we not ? one > more > thing I would like to say the reason I think you all know why I didn't > sue KOLB > is I still want to build a MKIII and I believe I will . first I need to > build > a shop and hanger in O'Brien the get a kit and work my way through it . in > 3or4or5 years maybe I will fly , MY wife says she won't stop me , WHAT A > WIFE > she is the reason I live . Thanks for all the good will you all wished > us back > in November Norm was lucky to have you all for friends . Sorry about the > long > story vie haven't had a computer fo a while . it would be great to hear > from > any of you any time . a KOLBER forever Chris davis cape cod ma.& O'Brien > Fl. > > > ________________________________________________________________________________
From: "Christopher Armstrong" <tophera(at)centurytel.net>
Subject: Chris Davis' Recovery
Date: Dec 13, 2005
I rarely read anything that inspiring. A real merry Christmas story that was. I wish your demo ride would not have gone wrong but I am very glad to hear that after what must have been a real tough year you are going to be able to get on with your life. And great job on the wife selection... bless her! I swear there is no greater thing then to have the love of a good spouse. Topher ________________________________________________________________________________
From: "Paul Petty" <Lynnp@c-gate.net>
Subject: kolbra012
Date: Dec 13, 2005
required 4.6, BAYES_44 -0.00, HTML_MESSAGE 0.25) Hi Kolbers, I second everyone in the hats off to Chris. Class act for sure. Bruce Chestnut is also a class act and I'm sure that he has been there although you rarely hear his name. Rather proud to get the "Hot Box" mounted thanks to Mark German for the bracket. http://www.c-gate.net/~ppetty/photos/PC110002.JPG Also Mark made me really nice brackets for the radiator. Fit perfect! http://www.c-gate.net/~ppetty/photos/PC110005.JPG http://www.c-gate.net/~ppetty/photos/PC110004.JPG Anyone have a photo of the part that connects the throttle cable to the Kolb quadrant? I ordered two from Travis today. Also ordered the cables and few remaining parts from Ronnie at South MS light aircraft. Getting Close gang! Paul Petty Building Ms. Dixie Kolbra/912UL/Warp I.L.D.S. ________________________________________________________________________________
From: "dama" <dama(at)mindspring.com>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
Thanks for sharing, Chris. We are all behind you and look forward to sharing some airspace with you someday... Kip Atlanta FSII ----- Original Message ----- From: "chris davis" <scrounge69(at)comcast.net> Subject: Kolb-List: NORMS MK3 CRASH ________________________________________________________________________________
From: robert bean <slyck(at)frontiernet.net>
Subject: Re: NORMS MK3 CRASH
Date: Dec 13, 2005
Chris, thanks for the update. Many of us were wondering about your progress. Better check and see if all that stainless doesn't swing a compass. -some's magnetic, some's not :) -BB > > ________________________________________________________________________________
From: N27SB(at)AOL.COM
Date: Dec 13, 2005
Subject: Re: NORMS MK3 CRASH
In a message dated 12/13/2005 4:43:15 PM Eastern Standard Time, scrounge69(at)comcast.net writes: > HI LIsters its been a year and a month since I was the passenger with Norm > at > the Kolb factory. Rest his soul, Chris, I would like to thank you for your attitude and your decision in regard to Norm and his family. I worked closely with Norm for a short period of time on a few projects and grew to love him very quickly. He helped so many people over that dangerous hurdle of transition from airplane to UL including myself that nobody really knows the total. I cherish the times that I flew with Norm and will remember them forever. Steve Boetto ________________________________________________________________________________
From: "Clay Stuart" <tcstuart(at)adelphia.net>
Subject: Norm's crash
Date: Dec 14, 2005
So glad to hear that Chris Davis is recovering and has such a noble outlook on his situation. Has Kolb addressed the fuel tank contamination problems that contributed to this accident? I had flown with Norm several times and found him to be such a meticulous pilot, I don't understand how the fuel problem evolved. Shouldn't the stock tanks be designed so that they can be readily sampled and fed through a gascolator to prevent these occurances? I have not touched my Mark IIIXtra project since Norm's accident, and may never finish. It had a profound effect on me. I had just been up with him at the fly-in right before the accident, and had teased his small girls. I made a sizeable contribution to the girls education fund and received a very nice note from his widow. Still hoping to fly again, but can't recover my enthusiasm. Clay Stuart Danville KY P.S. Chris, it was good to hear the nice things about the Univ of KY hospital. I spent 4 years there in dental school many years ago (33). ________________________________________________________________________________
Date: Dec 14, 2005
From: Larry Duncan <lariardo(at)centurytel.net>
Subject: Re: NORMS MK3 CRASH
________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Doctor! Doctor! My 503 is sick!/Fails to Fire Plugs
Date: Dec 14, 2005
| In order to get it | started, needs to be spun faster than even a new battery can spin it. | | John Jung John J/Gang: We had a similar problem with the first 912 I bought. Could not get it to fire. I was pulling my hair out trying to figure out what was wrong with this "piece of junk". The morning I was going to fly down to Ronnie Smith's, Lucedale, MS, to diagnose and fix the problem, I got an idea while in the shower. Figured if I closed the spark plug gap a bit it might start easier. As soon as I got to Ronnie's, 187 miles by air, I went to eat lunch. When I got back Ronnie had the problem fixed. He closed the spark plug gaps down to .020. Normal gap by the book is .028. After that it always fired right up like it was supposed to, except once at the Lake Texoma Flyin at Cedar Mills, TX, in 1998. Got ready to head for home and the 912 would not fire, period. Pulled the plugs, closed the gap back down to .020 and it fired right up. Have not had this problem with the 912S, however, I run the plugs at .025 when I put them in new and at 50 hours when I pulll to inspect and regap. Not a good feeling to be a long way from home with an engine that does not want to fire. I don't know if this is the problem or not. I don't know if you put new plugs in or not. But if it was me, I would put in new plugs and close the gap down to see if it would solve the problem. The 912 ran like a clock once it was started. Just a bugger to get it to fire.............................. john h MKIII/912ULS hauck's holler, alabama ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Kolb List: Doctor! Doctor! My 503 is sick!
Date: Dec 14, 2005
0.00 MANY_EXCLAMATIONS Subject has many exclamations Bryan and Group, That is a good question. The problem started after doing a de-carbon. But I thought that it was just a battery problem, so I didn't think further. Oh, I didn't change the plugs with the de-carbon, because they have less than 5 hours on them. Also, the compression seems the same. Only one broken oil ring was replaced and the engine showed no sign of significant wear with 200 hours. Although, it doesn't have many hours, it's probably 10 years since it was manufactured. John Jung John was the engine running fine and then one day it just started this or has something been changed on it? ________________________________________________________________________________
Date: Dec 14, 2005
From: possums <possums(at)mindspring.com>
Subject: Re: Doctor! Doctor! My 503 is sick!
Hey John http://media.putfile.com/Worst-Job-Ever How's Charlie doing? ________________________________________________________________________________
From: "Richard & Martha Neilsen" <NeilsenRM05(at)comcast.net>
Subject: Fuel System
Date: Dec 14, 2005
Clay/All I thought there was still some debate on the exact cause of the engine stoppage. I came from general aviation and every certified airplane has a fuel drain at the low part of the fuel system. Because of this I didn't feel comfortable with the Kolb recommended system. My fuel system uses the stock 5 gallon fuel tanks. I take fuel from the bottom of my tanks. Each fuel outlet has a finger strainer. The fuel lines tee together and feed directly to a aircraft gascolator. The gascolator is at the low point of the fuel system and it has a drain valve that sticks out the passenger side of the fuselage it is also equipped with a strainer. From the gascolator the fuel goes to a large automotive filter. After the filter it goes to my electric backup fuel pump and then to my primary electric fuel pump. From the fuel pumps the fuel goes thru a shout off valve and then to the carburetors. Each carb has its own strainer. Before I fly each day and after each fuel fill I drain some fuel from the gascolator. When I'm home I collect the drained fuel in a small clear glass jar so that I can see any junk or water in the fuel lines. When away from home I just drain some on the ground. I understand Norm's crash had a profound effect on you but life is dangerous. Just getting out of bed in the morning is a risk and you probably don't even give a second thought to getting in a car which is much more dangerous than flying. Just build in those safety features in your plane you feel necessary to reduce the risk. Come on you still have time to beat the guy on the left coast with that moose something named airplane into the air. Rick Neilsen Redrive VW powered MKIIIc ----- Original Message ----- From: "Clay Stuart" <tcstuart(at)adelphia.net> Subject: Kolb-List: Norm's crash > > So glad to hear that Chris Davis is recovering and has such a noble > outlook on his situation. > > Has Kolb addressed the fuel tank contamination problems that contributed > to this accident? I had flown with Norm several times and found him to be > such a meticulous pilot, I don't understand how the fuel problem evolved. > Shouldn't the stock tanks be designed so that they can be readily sampled > and fed through a gascolator to prevent these occurances? ________________________________________________________________________________
From: russ kinne <kinnepix(at)earthlink.net>
Subject: Chris Davis
Date: Dec 14, 2005
All Many comments about Chris Davis' comments on the crash that injured him so badly. I don't need to add more -- he is one superb human being and we're lucky to have him in our midst. Rick Neilson described his excellent fuel system -- IMHO he has taken, most prudently, just about every precaution he possibly could have, to avoid fuel contamination and a subsequent engine failure. I personally would be very reluctant to fly anything that did NOT have a sump-drain at the lowest point of the fuel system . And I will always drain a sample and examine it carefully before engine start. After that the only thing left is to fly defensively, keeping a safe landing area within reach whenever possible, if the engine should stop at any time . Can't always do that, of course, esp. during landings & T/O's. But I still remember being chastised for saying "keep within gliding range of the field on downwind, base and final" by people who wanted me to use a 3-degree glideslope on final, and simply hope the engine will never quit. Sorry, guys, but I'll fly my way. Safely. Why not? Merry Christmas to all! Russ Kinne ________________________________________________________________________________
From: "Paul Petty" <Lynnp@c-gate.net>
Subject: hose clamps
Date: Dec 14, 2005
required 4.6, BAYES_44 -0.00, HTML_50_60 0.10, HTML_MESSAGE 0.25) Kolbers, A while back I mentioned the Gates Power Grip hose clamps. Here is what they look like. http://www.c-gate.net/~ppetty/photos/PC130001.JPG http://www.c-gate.net/~ppetty/photos/PC130006.JPG Paul Petty Building Ms. Dixie Kolbra/912UL/Warp I.L.D.S. :-) ________________________________________________________________________________
From: John Jung <jrjungjr(at)yahoo.com>
Subject: Re: Kolb List: Doctor! Doctor! My 503 is sick!/Fails to Fire
Date: Dec 14, 2005
0.00 MANY_EXCLAMATIONS Subject has many exclamations "Thank you!" John Hauck. it was the plug gap. I went to the airport after lunch to check the plug gaps. My gaps measured about .020", and I am not sure why. I reset them to .015, and then rolled the plane out to give it a test. Turned the key and pumped the primer. Fired right up on the third pump. This is the way it used to run, and I am very happy that it was such an easy fix. I even started it with the prop, to confirm that it is back to normal. It bothered me that I had set the gaps to .020 when my 503 manual says .016 + - .02 (I'm sure they meant .002). I looked in my other source of Rotax information, the CPS catalog. Page 20 indicates a .02 in. electrode gap for a Rotax 503 dual ignition engine. John Jung Firestar II N6163J Surprise, AZ Original request: > I need some two cycle advise. I have a problem with my 503 that I have > never experienced before with any two cycle. In order to get it > started, needs to be spun faster than even a new battery can spin it. > It starts with jumper cables. Once started, it seems to run fine. I > even flew with it because I thought that I just had a battery problem. > It will start up normally right after being shut down, but not 15 > minutes later. When it fails to start, it will not fire at all and get > flooded from using the primer or the chokes. With jumpers on, and the > throttle opened, it will clear out, and fire up. The battery seems to > spin it as fast as it ever did. it spins much faster with jumpers. ________________________________________________________________________________
From: "John Hauck" <jhauck(at)elmore.rr.com>
Subject: Re: Doctor! Doctor! My 503 is sick!/Soot in the Spark Plug
Wire Caps


November 18, 2005 - December 14, 2005

Kolb-Archive.digest.vol-fq