RV-Archive.digest.vol-hu

January 19, 2000 - January 25, 2000



From: pcondon(at)csc.com
Date: Jan 19, 2000
Subject: Re: Wing Dimensions
> without the airlerons or flaps attached. Don't forget the attach brackets are part of the game even if you size without the flaps or ailerons......(Talking about the brackets that attach the ailerons...the flap is held in place with hinge......keep the pin in the hinge if your hinge is mounted-don't ask me how I know this. ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)mari.net>
Subject: Re: RV-6 Wing dimensions
Date: Jan 19, 2000
Hi Don't forget that you can leave your tank off too. That is what made it possible for me to get my wing out of my basement. Kept my wife happy too. Regards, Jeff Orear RV6A 25171 second wing Peshtigo. WI ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 19, 2000
Subject: Re: Norm closed press switch
"dont burn out and the brightness is easly set with the current limiting resisters".......Be careful those resisters get very hot but otherwise agree that LEDS are a great way to go for indicator lights & night lights. Come in various colors also. hsierra(at)flash.net on 01/19/2000 02:59:39 PM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: Norm closed press switch I just started mine, I have the canopy unlatched light done working on the flaps, and trim. I prefer to use LED's they are small, light weight, they dont burn out and the brightness is easly set with the current limiting resistor. i will be adding some pictures to my web site soon. www.flash.net/~hsierra just my 2c worth bob burns RV-4 N82RB s/n 3524 Along these lines who has done a good annunciator panel setup? I'm >wondering about proper impedence values do equalize the lights, a common >push to test button and where to connect for the various lights. (i.e. >starter on, fuel pump on, flaps down etc.) > > ________________________________________________________________________________
From: RV6junkie(at)aol.com
Date: Jan 19, 2000
Subject: Re: Seal Pack?
In a message dated 01/19/1970, 9:42:50 AM, rv-list(at)matronics.com writes: <> Seal Pack 316.942.6211 Part Number CS3200B 1/2 Gary Corde RV-6 N211GC-NJ ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 19, 2000
Subject: Re: RV-6 Wing dimensions
D O N " T F O R G E T T H E B R A C K E T S ________________________________________________________________________________
From: JusCash(at)aol.com
Date: Jan 19, 2000
Subject: Re: Off Subject Radio Question
Bob, you can get current and outdated installation manuals from------ ESSCO, INC. 426 W. Turkeyfoot Lake Rd. Akron, Ohio 44319 330-644-7724/Fax330-644-0886 E-Mail esscoeast(at)aol.com This info is in the Yeller Pages Cash Copeland In a message dated 1/19/00 5:22:36 PM GMT Standard Time, robert.armstrong(at)wcom.com writes: << This isn't RV related, but I'm hoping someone on the list might have some information. I'm trying to do a favor for a friend by wiring up an old Narco Mark 12B boat anchor as a receive-only hangar radio. Does anyone have a connection diagram for this radio? I've checked the archives and everywhere I can on the Internet but can't find one. The radio was removed from a Cessna T210 when the FCC regulations changed. Please respond off-list to Robert.Armstrong(at)wcom.com. Thanks! Bob RV-8AQ Rudder >> ________________________________________________________________________________
Date: Jan 19, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: Was Severe Weather; Now, trip plans
A couple of friends of mine are going to be flying our RV-6, RV-6A, and RV-8's from north Alabama out to New Mexico and Arizona during the first week of February. I already have Sedona, AZ on my list....... Sam Buchanan (getting backup batteries for the GPS....) "The RV Journal" http://home.hiwaay.net/~sbuc/journal Sam: I would like to get the SoCAL Wing of Van's Air Force to fly out and meet you. Almost every Sunday morning, several RVs fly somewhere for breakfast. I would love to make one of the breakfast fly-outs include your group. I will fly to Sedona for breakfast. Let us know a possible rendezvous location. My suggestion Big Bear City (L35). If you wish to fly as far west as California. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 19, 2000
Subject: Re: RV-6 Wing dimensions
Now getting the fuselage out of the basement is another story... ________________________________________________________________________________
From: JimRV6A(at)aol.com
Date: Jan 19, 2000
Subject: Re: Securing Fiberglass Nose Gear Faring
Paul Besing re: nose gear fairing-- On mine, I just riveted the hinge halves, same as on main gear, made the two pieces of hinge wire meet in about the center of the fairing (half way up to the cowling). I then used a hose clamp on the lower half. Works fine. Jim RV6A 30hr ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)mari.net>
Subject: Re: RV-6 Wing dimensions
Date: Jan 19, 2000
Mike: One thought for you before you go to the trouble with 4x8 sheets of ply......You can make a wood spar from some 2x4's and then temporarily attach 4 main ribs and 3 of the leading edge ribs. Support them with some baces on the tip and root ribs, and make a wooden rear spar to connect the main ribs. Also put wood spacers/supports between the leading edge ribs at thier tips. Then cover the whole works with paper. I have the advantage of living in paper country where I have access to rolls of paper that are 4 ft wide, but you could duct tape a bunch of newspapers together too. Making the mock-up this way was faster than doing it all in wood and was nice and light. I have a picture of mine if you would like for me to email it to you direct. Regards, Jeff Orear Rv6A 25171 Second wing Peshtigo, WI ________________________________________________________________________________
Date: Jan 19, 2000
From: Tim Houle <thoule(at)kneehill.com>
Subject: quickie on alodine
Can someone give me a good reason why if I alodine the internal parts I would need to also prime them. Isn't alodine enough corrosion protection? Tim Houle RV6 wings in dry old Alberta ________________________________________________________________________________
Date: Jan 19, 2000
From: Ed Holyoke <bicyclops(at)ecom.net>
"support(at)vansaircraft.com"
Subject: elevator stiffener mistake
I just did a dumb thing and drilled the upper outboard stiffener on the left elevator on the wrong side of the line. Instead of 1/8" overlap it's 1/8" clear of the matching stiffener and is inboard of it's intended location. Time for an new elevator skin? Ed Holyoke RV-6 #21531 ________________________________________________________________________________
Date: Jan 19, 2000
From: "Scott A. Jordan" <SAJ_SLJ(at)compuserve.com>
Subject: elevator stiffener mistake
Message text written by Ed Holyoke: >Instead of 1/8" overlap it's 1/8" clear of the matching stiffener and is inboard of it's intended location. Time for an new elevator skin?< I don't see how this is a problem. Having the stiffner 3/4" off from where the plans say it should be isn't a big deal. As long as the top and bottom stiffners don't hit you'll be fine. Save the money of a new skin for your next mistake! Scott A. Jordan 80331 / N733JJ ________________________________________________________________________________
From: Jim_Andrews(at)tivoli.com
Date: Jan 19, 2000
Subject: Re: elevator stiffener mistake
Ed, Don't be in too much of a hurry to replace your skin. I went through that with the horizontal stabilizer and now in retrospect wish I hadn't. The main reason for the over lap is to protect the skin from puncture when your bending the trailing edge to the proper taper. It also obviously provides rigidity to the elevator by acting like a rib. As long as you are careful and use some card board to protect the skin when your bending you will probably be ok. Just go with it and keep building ( that's what they keep telling me at Van's ). :-) - Jim RV-8AQ Wings N89JA ( reserved ) Ed Holyoke on 01/19/2000 04:45:43 PM Please respond to rv-list(at)matronics.com Subject: RV-List: elevator stiffener mistake I just did a dumb thing and drilled the upper outboard stiffener on the left elevator on the wrong side of the line. Instead of 1/8" overlap it's 1/8" clear of the matching stiffener and is inboard of it's intended location. Time for an new elevator skin? Ed Holyoke RV-6 #21531 ________________________________________________________________________________
From: Scott.Fink(at)Microchip.com.Wed, 19 Jan 2000 16:41:20.-0700(at)matronics.com
Subject: Re: elevator stiffener mistake
Date: Jan 19, 2000
01/19/2000 04:45:02 PM >I just did a dumb thing and drilled the upper outboard stiffener on the left elevator on the wrong side of the line. Welcome to the club! >Time for an new elevator skin? That is up to you, if it is on the bottom, I would just dimple it and put in another rivit, and probably nobody would notice it if you did the same if it is on the top. If on the top you could do the rivit and then fill in around the head later before painting and it will be invisible. Best Regards, Scott Fink Done my share of dumb things! ________________________________________________________________________________
From: "Michael Robertson" <mrobert569(at)hotmail.com>
Subject: Re: fuel line holes
Date: Jan 19, 2000
Earl, Too late (of course) I figured that I should have gone with the bulkhead fittings instead of the grommets. Be as it may I installed the grommets bit. The grommets were in the same bag as my fuel line fittings. The hole thru the side wall came out to about one inch. If you haven't made holes yet then go with the bulkhead fittings. Mike Robertson RV-8A >From: EARL FORTNER <e.fortner(at)worldnet.att.net> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: fuel line holes >Date: Tue, 18 Jan 2000 19:43:25 -0500 > > >What size holes have you guys cut in the fuse for fuel lines from wing >tanks and what size gromets did you use if any to prevent chafing of >fuel line? > >Earl still trying to plumb the 4 > > ________________________________________________________________________________
From: "Michael Robertson" <mrobert569(at)hotmail.com>
Subject: Re: Cracked Elevator Skin
Date: Jan 19, 2000
Jeff, Join the club. I think more people have had this problem than the successful ones. Most people that have done this have gone ahead and cut off the flaps and, using a piece of wood as a former, made a small rib. Then just rivet it in with the web of the rib facing toward the trim tab and rivet it in with blind rivets. I think it actually looks better this way. Good Luck! Mike Robertson RV-8A QB >From: Jeff Point <jpoint(at)execpc.com> >Reply-To: rv-list(at)matronics.com >To: RV List >Subject: RV-List: Cracked Elevator Skin >Date: Tue, 18 Jan 2000 19:10:00 -0600 > > >Somebody save me! > >On the left elevator skin, while bending the little tabs in the skin for >the trim tab cut out, I managed to develop a small crack in the skin. >The crack is 1/4 inch back from the forward edge of the tab, and runs >spanwise, parallel to the trim tab spar, about 3/8 inch long. Since it >is in a non-structural area, I would think that I could drill stop it >and forget it. Any advice, or better ideas how to fix it, besides a new >elevator? Oh, and of course I had the whole forward edge of the thing >riveted before I figured this out. > >And everything was going SOOOO smoothly on the elevators! > >Jeff Point >jpoint(at)execpc.com >-6 elevators, waiting on wings >Milwaukee, WI > > ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Vetterman Exhaust Supports
Date: Jan 19, 2000
Do not be offended, but if you had trouble with your hinges too you may have a vibration problem. -----Original Message----- From: Larry Pardue <n5lp(at)carlsbad.net> Date: Monday, January 17, 2000 8:37 PM Subject: RV-List: Vetterman Exhaust Supports > >Listers, > >I already know I am mister break it when it breaks for no one else, but has >anyone else had trouble with the exhaust support pieces in the otherwise >excellent Vetterman exhaust pipe kit? > >In about 120 hours I have had the adell clamps break four different times >and one of the flattened steel tubing pieces break once. Is it an >installation or a materials problem? > >My only ideas on solutions at this point are heavier wall steel tubing and >some kind of two piece plumbing part to replace the aluminum adell clamps. > >Now that I think I have replaced all the troublesome cowl hinges on my >airplane, this seems to be the next part that I am always having to fix when >I would much rather be flying. Whee! > >On every preflight I am dreading the shaking of the exhaust pipes. > >Larry Pardue >Carlsbad, NM > >RV-6 N441LP > > ________________________________________________________________________________
From: "John Devlin" <jdevlin(at)americus.net>
Subject: Re: Gas Cap Engraving
Date: Jan 19, 2000
Steve, I sent mine Tuesday from south Georgia. You should see them very soon. BTW, what do you charge? I will put a check in the mail as soon as I know the amount. Thanks, John Devlin ----- Original Message ----- From: <PANELCUT(at)aol.com> Sent: Wednesday, January 19, 2000 9:41 AM Subject: Re: RV-List: Gas Cap Engraving > > Tom and Listers > > This is the last week for those that have not got there caps in. I will > start them Monday. Sorry about the delay but would like to give a few people > who have told me they sent their caps time to get here. For those who want to > send them that haven't now is the time to do so. If they are a little late > that's OK but prefer you send them NOW. Listed below are the one's I have > received so far. I also have a few that were redo's from last time that will > be done with this batch I hope this hasn't delayed anyone but I just decided > to do all when I set them up. > > John Warren > Bill Gibbs > Robert Acker > Craig Weiler > Jim Wendel > Kevin Belue > David Plerson > Tom Ervin > Dale Wotring > Pete Bodie > Mel Jordan > Gerald Forrest > Randy Pflanzer > Steven Cole > Scott Chambers > Curtis Shoemaker > > Thanks > Steve Davis > > ________________________________________________________________________________
From: "Jerry Carter" <rv8abuild(at)mindspring.com>
Subject: Re: Crate Sizes...
Date: Jan 19, 2000
----- Original Message ----- From: The Von Dane's <vondanes(at)hotmail.com> Sent: Wednesday, January 19, 2000 5:46 PM Subject: RV-List: Crate Sizes... > > I was trying to find the crate sizes for the wings, fuse, and finish > kits on Van's new site, and could not... Anyone have the sizes, or > where I can find them? I don't have the sizes, but I'll be happy to send you jpeg pictures of the fuselage and wing crates loaded on a 16 foot trailer if that will help you. Just let me know if that would help. Jerry (I Take Pictures Of Everything) Carter RV-8A > > ________________________________________________________________________________
From: "Tim Lewis" <timrv6a(at)earthlink.net>
Date: Jan 19, 2000
Subject: Re: Securing Fiberglass Nose Gear Faring
On 18 Jan 00, at 20:47, Paul Besing wrote: > > I just purchased a nose gear faring from George Orndorff, and was curious > to know how builders attach this. Does it need to be filled with foam, > ala the main farings that the rocket guys sell? Are rivets applied to the > trailing edge? I attached the fairing (from Van's) via hose clamp at bottom, and riveted tabs to the top of the fairing. The tabs are held to the nose gear via another hose clamp. Rather than fabricate an intersection fairing on the cowling, I fabricated one that is part of the nose gear fairing. Picture is at http://www.geocities.com/timrv6a/finish2.htm Tim ****** Tim Lewis -- Springfield VA RV-6A N47TD - First Flight 18 Dec 99 TimRV6A(at)earthlink.net http://www.geocities.com/timrv6a ________________________________________________________________________________
Date: Jan 19, 2000
From: Al Mojzisik <prober(at)iwaynet.net>
Subject: Re: Lycoming O-360 F1A6 for my RV-8A?
Bill, I don't know if the F1A6 is like the IO-360-C1C sump but if it is, there is a boss on the front of the sump that can be machined so that it will accept the throttle body (on the -IO) or Carb. effectively moving it to the front of the sump. On the other hand you may just be able to change the oil sump and make it an A1A. For the non-fuel injected engines that usually costs $350 or maybe an even trade for your sump if you find someone in the pusher crowd (Long EZ, Cozy, or Velocity.) who is looking for your sump. AL > >Hi all... > >I am interested in buying a Lycoming O-360 F1A6 for my RV-8A. > >It came out of a 172RG. I believe it has the carb mounted on the rear of >the sump. > >Can anyone tell me if, in fact, this engine will work in an RV-8A? And what >may need to be done to it to make it fit? And how much this may cost? > >Thanks in advance... > >-Bill Von Dane - Colorado Springs, CO >RV-8A N912V res., waiting for wings >http://vondane.tripod.com > > ________________________________________________________________________________
Date: Jan 19, 2000
From: n3773 <n3773(at)mciworld.com>
Subject: hemostats, elevator bolts
For rudder and elevator bolts buy a hemostat with the 45 degree jaws. Bend the jaws out about 90 degrees, insert a -3 nut and clamp them in a vise. Pound the tips closed. These will grip nuts and bolts very well and the angled jaws will get into more spaces than the straight ones. For shim washers tape the washer to the middle of some masking tape. Use the tape "handles to position the washer. Pierce the washer with the bolt, pull on the tape to tear and remove. I have also found the ratcheting closed end wrenches are great for quickly tightening these bolts. Kevin -6a ________________________________________________________________________________
Date: Jan 19, 2000
Subject: Re: : 6A tip-up canopy frame fit.
From: Blah ba Blah <daviddla(at)juno.com>
Steve, for the strut stop you just bolt a piece of metal to the fuselage sill plate. located so that the forward section of the strut that is attached to the tip up will contact just before the top is completely down. This is adjusted to prevent the strut from pushing the canopy frame forward when in the closed position. I came across a picture that showed the stop in some paperwork sent with the kit regarding the fiber glassing of the forward canopy frame. David Ahrens ________________________________________________________________________________
From: Gusndale(at)aol.com
Date: Jan 19, 2000
Subject: Re: elevator stiffener mistake
In a message dated 01/19/2000 3:03:10 PM Pacific Standard Time, bicyclops(at)ecom.net writes: > I just did a dumb thing and drilled the upper outboard stiffener on the > left elevator on the wrong side of the line. Instead of 1/8" overlap > it's 1/8" clear of the matching stiffener and is inboard of it's > intended location. > Time for an new elevator skin? > > Ed Holyoke > RV-6 #21531 Ed, If the hole is clear of everything you can just dimple it and put a rivet in it. Problem solved. There aren't any structural issues to worry about. You would have to be a real perfectionist to reject the skin for that one error. If you are like most of us, you will soon come to the conclusion that with small errors like this it's best just fix it and move on. You'll still have a great airplane and even you won't notice that extra rivet a year from now. Best Regards, Dale Wotring ________________________________________________________________________________
Date: Jan 19, 2000
From: James Freeman <cd005677(at)mindspring.com>
Subject: Panel planner/RV-8
Listers--I got paranoid after Randy's heads up warning about Panel Planner and printed my entire panel out full size and taped it onto the actual aluminum piece from the kit. I used an Epson SC 800 printer and a Compaq Presario 5304 running windows 98. I used default settings for everything (no scaling) The vertical dimension does not account for the bend at the bottom of the panel. When you take this flange (5/8") and the bend radius you get the 3/4" discrepancy Randy noted. The paper pattern fits -perfectly-, but it wraps around the flange to the edge. If you hold the panel up to a light, the pre-punched holes are exactly where they are indicated on the pattern. The only actual instrument I have to hold up to the pattern is the Rocky Mountain micro-encoder, but it is dead accurate. The faces of the RC Allen electric gyros print 3.25" tall, the other 31/8" instruments appear to be about 1/16 small. The 2.25" instruments are all 2.25" The radios are exactly right according to the manufacturers' web sites, as is the Rocky Mountain monitor. I suspect that the template was taken directly from Vans' cutting CAD/CAM file, without taking the bend into account. I also agree with the observation that many printers amy not scale accurately. Thanks Randy for the warning--I think we should all print first, before ordering YMMV James Freeman RV-8Q fuse ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: RV8-List: Custom Canopies
Date: Jan 19, 2000
This must be a change, as mine has no discernable tint, got it about 2 years ago. Alex Peterson 6A > The canopy that comes in Van's finish kit is tinted, slightly. ________________________________________________________________________________
From: Wndwlkr711(at)aol.com
Date: Jan 19, 2000
Subject: Re: jig available in Phoenix, AZ USA
Tom, if the jig for the RV6 is still available I am interested. I live near Blythe, CA, but can make the drive this weekend. Let me know. George Stanley RV-6A Finishing wings ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
Subject: RE: RV3-List: rv3 fuselage fuel tank
Date: Jan 19, 2000
Gary- I doubt that it's too much pressure from the ram vent. The old tanks were riveted as mentioned by Jim, and integral with the top forward skin (.040 vs. .025 for welded tanks or wing tanks). The welded tanks, to my knowledge, never had the inverted "V" baffle for inverted pickup, but rather went to an open welded tank with/without a flop tube as per post 1984 RV-3 plans. I have read in past newsletters of the RV-3 that there have been forced landings due to the improper orientation of the fuselage fuel tank vent/pressurization tube (newsletter #17, March 1978). It mentioned only briefly that the vent can be mounted neutral/static, but to develop full power on some carb/injector installations, that it needs to be mounted in a ram air orientation per plans. There's an interesting write up by Van on the gravity feed fuselage fuel plumbing in the RVator #21 March 1980. It discusses the use of a 1/4" return line from the carb back to the strainer/tank. It appears to be a "recirculation" path for fuel from the carb. This was used with an internal flop tube and so that fuel that continued to be pumped from the engine driven pump into the carb fed by the flop tube. . .drained back through the system if too much fuel was introduced to the carb during unusual aerobatic maneuvers, etc. Without the return line with the flop tube, Van stated that the carb got too much fuel and during aerobatic attitudes and reduced performance. Rob Reece RV-3 SN45 re-skinning wings, what a shame to have to put wings BACK into the darn jigs again!!! Socorro, NM ________________________________________________________________________________
From: RV8DRIVER(at)aol.com
Date: Jan 20, 2000
Subject: Re: Severe Weather
Migosh larry, I know just how you feel. Why just the other day it was so cold in the garage (maybe 70) I had to open the double-wide door to warm things up. Suffering in So Fla. Andy Johnson, Boca Raton Well I could get some work done on my airplane if the darn weather was just a little better. Temps have been running around 77-80 degrees. I really prefer about 72 degrees. While flying at 6,000 MSL yesterday I was running the vents full tilt and was still a bit warm. I think I saw a cloud too.snip Larry Pardue Carlsbad, NM< ________________________________________________________________________________
From: "Graham Jones" <gratech(at)a1.com.au>
Subject: Re: Palm GPS units
Date: Jan 20, 2000
Colours nice guys, but you have to havethe right type of screen. I was looking at the E100 the other day and the HP Jornada as well. It's high summer here in OZ and the day was around 31C (100+F) ie. REAL BRIGHT!. Took the handhelds out side and couldn't read the screen at all. They just turned black!. Took the mono Compaq Aero (?) and the Casio E15 (16 grey scales)outside and they didn't change a bit...... Seems that the latest techno isn't so great - except where you pay heaps for it like in the Garmin GNS430 etc. Graham Jones (SUNNY!) Australia ----- Original Message ----- From: Greg Yotz <greg(at)controlvision.com> Sent: Wednesday, January 19, 2000 2:42 AM Subject: Re: RV-List: Palm GPS units > > To bad the Fuel Manager didn't have sensors for real updates. > Has anybody seen a Palm Pilot at night inside the cockpit? > I like the looks of the Casio E-100 PDA. It looks good and is color. > > I still like the color GPS Moving map at <http://www.controlvision.com> > > Greg > > > -----Original Message----- > From: Shelby Smith <shelbyrv6a(at)mindspring.com> > To: rv-list(at)matronics.com > Date: Sunday, January 16, 2000 10:11 PM > Subject: RV-List: Palm GPS units > > > > > >A while back there was a discussion on the Palm units. > > > >I found this website with more information. > > > >FYI only. I am not advertising for them, but they are getting my attention. > > > >http://www.aspenleaf.com/palm/ > >-- > >Shelby Smith > >shelbyrv6a(at)mindspring.com > >RV6A - Skinning Fuselage - 200HP > >N95EB - reserved > > > >---------- > > > > > > ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: fuel line holes
Date: Jan 20, 2000
If you go with bulkhead fittings, what kind of flexible line must you use between the wing tank and the bulkhead fitting? Steve Soule Huntington, Vermont RV-6A Panel, wiring and fuel hookups -----Original Message-----Too late (of course) I figured that I should have gone with the bulkhead fittings instead of the grommets. Be as it may I installed the grommets bit. The grommets were in the same bag as my fuel line fittings. The hole thru the side wall came out to about one inch. If you haven't made holes yet then go with the bulkhead fittings. ________________________________________________________________________________
From: "Rick Caldwell" <racaldwell(at)hotmail.com>
Subject: Post-1st Flight Inspection
Date: Jan 20, 2000
I thought maybe someone could benefit for this. After my first flight, I have found these items that need fixing. 1. The top skin (glaresheild) was painted flat black and then riveted. The rivet heads have a bad reflection on the windshield. I'll paint these rivets with flat black paint. This would have been easier before I put in the windshield. 2. Pipe threads are hard to seal. I mounted my fuel flow transducer on the firewall. A straight fitting was used on the inlet and a 90 elbow on the exit. In order to get the elbow pointed forward, it was not fully tight. Thread sealant was used on all pipe threads. Green stains were on the transducer after the first flight, indicating a fuel leak. Last night I removed the transducer & tighten the fitting. Fully tight, it was pointed aft onto the firewall. I removed the fitting and retightened several times. Each time the fitting turned more toward the front. With some serious tightening, the fitting is facing forward and no leaks with the system pressurized. Also the pipe fitting on the oil pressure tranducer was leaking. This fitting was very tight. I removed it and tightened it again. Next run will determine if it is leakproof. 3. The brake fluid reservoir was filled to the top while the -6 was sitting 3-point. After the flight, brake fluid was all over the firewall under the reservoir and down the belly. Guess the reservoir should only be half full. 4. The carb temp sensor for the RMI uMonitor has a green stain around it. I'll remove it tonight and put some thread sealant on the threads. Rick Caldwell RV-6 N136RC 1.3 hrs Melbourne, FL ________________________________________________________________________________
From: Rv8don(at)aol.com
Date: Jan 20, 2000
Subject: Re: Panel planner/RV-8
In a message dated 1/19/00 11:13:29 PM Eastern Standard Time, cd005677(at)mindspring.com writes: << The vertical dimension does not account for the bend at the bottom of the panel. >> I came across this "oversize" problem with the RV-8 panel diagram some time ago. I just ended up drawing a line across the bottom to account for the flange and designed away. I brought this up to the panel planner people nearly a year ago. I guess they haven't yet done anything about it. -Don RV-8 NJ ________________________________________________________________________________
Date: Jan 20, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: Post-1st Flight Inspection
--- Rick Caldwell wrote: > > 3. The brake fluid reservoir was filled to the top > while the -6 was sitting > 3-point. After the flight, brake fluid was all over > the firewall under the > reservoir and down the belly. Guess the reservoir > should only be half full. > > > Rick Caldwell > RV-6 N136RC 1.3 hrs > Melbourne, FL > Rick: After 490 flying hours, I can say that I fill the reservoir between 1/2 and 3/4 for the same reason. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Post-1st Flight Inspection
Date: Jan 20, 2000
> >I thought maybe someone could benefit for this. After my first flight, I >have found these items that need fixing. On the topic of leaks, here's what I've had so far in 17.5 hours: 1. Also had brake fluid on the firewall and streaming back on the belly. I had overfilled it as well. It's now about 2/3 full, but still urped up some juice after a momentary spell of ballistic flight. (I dig that weightless feeling). I would think a fully inverted capable airplane would have quite a mess here after spending more substantial periods of time at negative G. 2. The intake tube rubber boot on cylinder #1 wasn't sealing and yesterday I noticed some blue fuel stains on the inside of the cowling. I found the Breeze clamps needed some tightening. We'll see how it does today. I need to share in Larry's icky flying weather here in the Land of Enchantment...temps around 80 are forecast down south. :) 3. I have one seeping rivet in the bottom of the left tank at a stiffener. Bummer. Out comes the Proseal when I'm done flying for the week. At least it isn't painted yet. 4. Air leaks around the back of the canopy skirt. I've been adding small strips of adhesive backed felt and it's getting better. Most of it comes in through the square hole cut in the skirt to fit over the slider rail. 5. I had brake fluid leaks at the el cheapo brass swamp cooler type fittings at the master cylinders. These would not seal worth a darn even after replacing the inserts and compression nuts. I replaced the fittings with stainless Swagelok fittings. NO leaks and a MUCH better choice for such a critical fitting. That's about it. The belly is staying pretty clean so at least the engine isn't splooging out large amounts of oil and water vapor. The breather was repositioned over one of the exhaust pipes and this seems to be helping to burn off the stuff it does send overboard. All in all, life is good, it flies great and I'm having a ball! Brian Denk RV8 N94BD where to fly to today? Hmm... ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: Re: fuel line holes
Date: Jan 20, 2000
You could go either way really. I went with Earl's steel braided hose. Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit ----- Original Message ----- From: "Stephen J. Soule" <SSoule(at)pfclaw.com> Sent: Thursday, January 20, 2000 6:28 AM Subject: RE: RV-List: fuel line holes > > If you go with bulkhead fittings, what kind of flexible line must you use > between the wing tank and the bulkhead fitting? > > Steve Soule > Huntington, Vermont > RV-6A Panel, wiring and fuel hookups > > -----Original Message-----Too late (of course) I figured > that I should have gone with the bulkhead > fittings instead of the grommets. Be as it may I installed > the grommets > bit. The grommets were in the same bag as my fuel line > fittings. The hole > thru the side wall came out to about one inch. If you > haven't made holes > yet then go with the bulkhead fittings. > > ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: Panel planner/RV-8
Date: Jan 20, 2000
> The vertical dimension does not account for the bend at the bottom of > the panel. When you take this flange (5/8") and the bend radius you get > the 3/4" discrepancy Randy noted. The paper pattern fits -perfectly-, > but it wraps around the flange to the edge. If you hold the panel up to > a light, the pre-punched holes are exactly where they are indicated on > the pattern. > > The only actual instrument I have to hold up to the pattern is the Rocky > Mountain micro-encoder, but it is dead accurate. > > The faces of the RC Allen electric gyros print 3.25" tall, the other > 31/8" instruments appear to be about 1/16 small. > > The 2.25" instruments are all 2.25" > > The radios are exactly right according to the manufacturers' web sites, > as is the Rocky Mountain monitor. > > I suspect that the template was taken directly from Vans' cutting > CAD/CAM file, without taking the bend into account. I also agree with > the observation that many printers amy not scale accurately. > > Thanks Randy for the warning--I think we should all print first, before > ordering James, Great post, and good find on the flange issue. This of course makes sense when you think about where they got the panel drawing... from Van's part drawing. Now you've got me curious... I will go back and print out a full size print again and see how it compares with the unbent flange allowed for. The instrument scaling errors I noted were probably the worst on the Electronics International gauges. They use a 2.25" hole so you could just check the dimension without the actual instrument if you like. BTW, if you plan on using the EI gauges they have a square case that is exactly 2.5". You can then use 2.5" centers for your holes which of course yields zero clearance between them. This is a good thing because then then provide support for each other. In fact I may link a couple of zip ties and wrap the bundle of cases to elminate any potential vibration between them. My panel is now fully cut so the Panel Planner issue is a bit moot for me. For others such as yourself another thing you need to watch for is the overlap of the rear panel (F-803 something) onto the back of the main panel. You will find that this get's in the way. I can't think of a way to allow for this precisely when working in Panel Planner, but once you have a full size drawing you could easily draw a line inboard the proper distance (I think it's just over an inch - at work right now) to make sure all of your items clear it. Of course you're most concerned about the cases on the back of the panel which you may not have yet. I will keep my web site updated with my panel progress. It now shows the main cutouts and tonight I may finish the avionics rack portion and shoot a picture. Randy Lervold RV-8, #80500, panel, canopy skirt, etc. www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
From: "Linzel G . Civ - 43CES/CECP" <Gray.Linzel(at)pope.af.mil>
Subject: RV3 Mode of Operation Comparison
Date: Jan 20, 2000
I am wondering how many RV3 builders are content to fly with the older unmodified wings? While generally not of competition form, it seems I can comfortably/smoothly perform loops, rolls and most variations thereof without exceeding 160 MPH or the normal category G limits much less the utility category limits. The RV3 I built may have been one of the last ones shipped before the production hold. It's a fairly light, bare bones copy with a 160 lb pilot. I think I remember hearing a statement made that no RV3's have had catastrophic wing problems while being flown by their builder? Gray (like the color of my unpainted RV3) ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 20, 2000
Subject: fuel line holes
I would use either solid line with a vibration loop or the aeroquip flex that Vans has. I like the bulkhead method because it adds a solid tie point. The flex option allows the bent fittings ( 45 & 90 degree) to be used. A little more expensive but inthe large picture of building expenses- a drop in the bucket... SSoule(at)pfclaw.com on 01/20/2000 08:28:40 AM Please respond to rv-list(at)matronics.com Subject: RE: RV-List: fuel line holes If you go with bulkhead fittings, what kind of flexible line must you use between the wing tank and the bulkhead fitting? Steve Soule Huntington, Vermont RV-6A Panel, wiring and fuel hookups -----Original Message-----Too late (of course) I figured that I should have gone with the bulkhead fittings instead of the grommets. Be as it may I installed the grommets bit. The grommets were in the same bag as my fuel line fittings. The hole thru the side wall came out to about one inch. If you haven't made holes yet then go with the bulkhead fittings. ________________________________________________________________________________
Date: Jan 20, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: 40 Amp Wire Size
> >I have a stretch of wire going from my alternator breaker to my buss. It >will only be about 2 inches. I know the whole wire size chart thing, but it >doesn't really state what size wire will handle that kind of current. Could >I do it with 12 gauge? A bit light for 40A . . . how about a strip of brass or copper used to extend your bus bar to the alternator breaker . . . better yet, how about getting the fat breaker off the panel entirely and feed alternator output into the system via the hot side of the starter contactor. Thats how we're going to do it on the next model change to the Bonanza . . . Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
From: "Evan&Megan Johnson" <evmeg(at)snowcrest.net>
Subject: Re: RV3-List: RV3 Mode of Operation Comparison
Date: Jan 19, 2000
I recently had a conversation with Tom at Vans about this subject. I was bummed about the cost of the new wing since I only have a couple of hundred dollars into my kit. I was trying in vain to get him to tell me I could buy just parts of the new wing kit (spar strips) and substitute them for the old ones in my kit. My kit is very old #68....so I even have the thinner flat bar for the spar strips. After mentioning that I felt compelled to buy the new wing because I didn't want to die in this thing, he straightened me out. In his opinion there is nothing at all wrong with even the oldest wing design. As long as the pilot keeps within the G limits. As I am a very conservative pilot and have no intention of ever doing any aerobatics, it was agreed that the original wing design is more than sufficient. There are a whole lot of these things flying presently with no problems at all. The few that have come down have been reputed to be doing some pretty serious maneuvers. While I am planning on doing the simple modifications per the later plans, I am convinced that buying the new wing is not necessary. The only really big advantage in my view is in resale value. I probably wont ever sell it any way. Evan.....skinning first wing ----- Original Message ----- From: Linzel G . Civ - 43CES/CECP <Gray.Linzel(at)pope.af.mil> Sent: Thursday, January 20, 2000 8:36 AM Subject: RV3-List: RV3 Mode of Operation Comparison > --> RV3-List message posted by: "Linzel G . Civ - 43CES/CECP" > > I am wondering how many RV3 builders are content to fly with the older > unmodified wings? > While generally not of competition form, it seems I can comfortably/smoothly > perform loops, rolls and most variations thereof without exceeding 160 MPH > or the normal category G limits much less the utility category limits. > The RV3 I built may have been one of the last ones shipped before the > production hold. It's a fairly light, bare bones copy with a 160 lb pilot. > I think I remember hearing a statement made that no RV3's have had > catastrophic wing problems while being flown by their builder? > > Gray > (like the color of my unpainted RV3) > > ________________________________________________________________________________
From: TRAASHMAN(at)webtv.net (Joe Waltz)
Date: Jan 20, 2000
Subject: Panel holes
The 8 panel is geting a bit crowded. What is the min. separation between instr. that anyone has used successfully on the stock panel and/or any other thicker upgrades? ________________________________________________________________________________
From: "Stephen J. Soule" <SSoule(at)pfclaw.com>
Subject: fuel line holes
Date: Jan 20, 2000
It seems to me that the bulkhead fitting also lets you be a little less fussy about where the fuel line exits the fuselage. As designed, the fuel line has to come out and be precisely lined up with the fuel outlet on the wing tank. By using a bulkhead fitting, you have more freedom about where you locate the fitting because you are going to run a flexible line or a solid line with a loop to the wing. BTW, how much space is there between the wing and the side of the fuselage. I once had my wings on when I drilled the landing gear mounts, but I did not make a note of the width of that space. Steve Soule Huntington, Vermont RV-6A -----Original Message-----I would use either solid line with a vibration loop or the aeroquip flex that Vans has. I like the bulkhead method because it adds a solid tie point. The flex option allows the bent fittings ( 45 & 90 degree) to be used. A little more expensive but inthe large picture of building expenses- a drop in the bucket... ________________________________________________________________________________
From: "Doug Weiler" <dougweil(at)pressenter.com>
Subject: Powersport rotary engine
Date: Jan 20, 2000
Fellow Listers: Got a call today from Ray Richardson, president of Powersport Aviation. Ray has a position open at their facility in Osceola, WI to finish their RV-6A with their new rotary engine. They also have a Glastar kit which they would like to complete also. This could be a good thing for someone looking for a career change involving sport aviation. Also he would consider someone locally to work on these projects on a part-time hourly basis. Osceola is located 40 miles NE of St. Paul, MN. If you know of anyone interested, Ray's number is 715-294-2557. Thanks Doug Weiler, pres MN Wing =========== Doug Weiler Hudson, WI 715-386-1239 dougweil(at)pressenter.com ________________________________________________________________________________
Date: Jan 20, 2000
From: "Bob U." <r.r.urban(at)worldnet.att.net>
Subject: Re: RV3-List: RV3 Mode of Operation Comparison
Wouldn't it be interesting to know if those that broke wings in the past would not break this NEW wing as well? This is no reflection on this new wing what-so-ever, but there will be those that find themselves outside the limits..... of even of this new wing. Bob Urban ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Evan&Megan Johnson wrote: > > --> RV3-List message posted by: "Evan&Megan Johnson" > > I recently had a conversation with Tom at Vans about this subject. I was > bummed about the cost of the new wing since I only have a couple of hundred > dollars into my kit. I was trying in vain to get him to tell me I could buy > just parts of the new wing kit (spar strips) and substitute them for the old > ones in my kit. My kit is very old #68....so I even have the thinner flat > bar for the spar strips. After mentioning that I felt compelled to buy the > new wing because I didn't want to die in this thing, he straightened me out. > In his opinion there is nothing at all wrong with even the oldest wing > design. As long as the pilot keeps within the G limits. As I am a very > conservative pilot and have no intention of ever doing any aerobatics, it > was agreed that the original wing design is more than sufficient. There are > a whole lot of these things flying presently with no problems at all. The > few that have come down have been reputed to be doing some pretty serious > maneuvers. While I am planning on doing the simple modifications per the > later plans, I am convinced that buying the new wing is not necessary. The > only really big advantage in my view is in resale value. I probably wont > ever sell it any way. > Evan.....skinning first wing > ----- Original Message ----- > From: Linzel G . Civ - 43CES/CECP <Gray.Linzel(at)pope.af.mil> > To: RV3-List Digest Server > Sent: Thursday, January 20, 2000 8:36 AM > Subject: RV3-List: RV3 Mode of Operation Comparison > > > --> RV3-List message posted by: "Linzel G . Civ - 43CES/CECP" > > > > > I am wondering how many RV3 builders are content to fly with the older > > unmodified wings? > > While generally not of competition form, it seems I can > comfortably/smoothly > > perform loops, rolls and most variations thereof without exceeding 160 MPH > > or the normal category G limits much less the utility category limits. > > The RV3 I built may have been one of the last ones shipped before the > > production hold. It's a fairly light, bare bones copy with a 160 lb > pilot. > > I think I remember hearing a statement made that no RV3's have had > > catastrophic wing problems while being flown by their builder? > > > > Gray > > (like the color of my unpainted RV3) > ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Jan 20, 2000
Subject: Re: elevator stiffener mistake
Check with Van's to be certain but my guess is they will tell you to forget it and move on. ________________________________________________________________________________
From: "Michael Robertson" <mrobert569(at)hotmail.com>
Subject: Re: 40 Amp Wire Size
Date: Jan 20, 2000
Bob, Help me here. I read what you said several times but for some incredulous reason I can't comprehend it. Could you please forgive my density and explain fully. And how will this effect/tie into an external voltage regulator?? Mike Robertson RV-8A QB >From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: Re: RV-List: 40 Amp Wire Size >Date: Thu, 20 Jan 2000 10:36:13 -0600 > > > > > > >I have a stretch of wire going from my alternator breaker to my buss. It > >will only be about 2 inches. I know the whole wire size chart thing, but >it > >doesn't really state what size wire will handle that kind of current. >Could > >I do it with 12 gauge? > > A bit light for 40A . . . how about a strip of brass or copper > used to extend your bus bar to the alternator breaker . . . better > yet, how about getting the fat breaker off the panel entirely > and feed alternator output into the system via the hot side of > the starter contactor. > > Thats how we're going to do it on the next model change to the > Bonanza . . . > > > Bob . . . > > http://www.aeroelectric.com > > ________________________________________________________________________________
From: "Bill & Debi VonDane" <vondanes(at)hotmail.com>
Subject: Re: Powersport rotary engine
Date: Jan 20, 2000
Here is the URL of their web site: http://www.powersportaviation.com/ Bill Von Dane, Colorado Springs, CO RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com Fellow Listers: Got a call today from Ray Richardson, president of Powersport Aviation. Ray has a position open at their facility in Osceola, WI to finish their RV-6A with their new rotary engine. They also have a Glastar kit which they would like to complete also. This could be a good thing for someone looking for a career change involving sport aviation. Also he would consider someone locally to work on these projects on a part-time hourly basis. Osceola is located 40 miles NE of St. Paul, MN. If you know of anyone interested, Ray's number is 715-294-2557. Thanks Doug Weiler, pres MN Wing =========== Doug Weiler Hudson, WI 715-386-1239 dougweil(at)pressenter.com ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Post-1st Flight Inspection
Date: Jan 20, 2000
Brian, Any tips, in hindsight, on tank sealing? I'm currently wrestling with proseal myself. Larry Bowen RV-8 tanks Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Brian Denk > Sent: Thursday, January 20, 2000 10:00 AM > 3. I have one seeping rivet in the bottom of the left tank at a > stiffener. > Bummer. Out comes the Proseal when I'm done flying for the week. > At least > it isn't painted yet. > Brian Denk > RV8 N94BD > where to fly to today? Hmm... ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 20, 2000
Subject: Re: RV3-List: RV3 Mode of Operation Comparison
With all the best of intentions NOT to pull the G's on the rv-3 to place your butt in harms way what about a unintentional or otherwise sloppy manuver exit where you place your aircraft in a position where a breakup might occur.......I would probably go with the wing mod AND fly safe with the safety margin the newer wing offers. You could bang out a set of wings while you fly your 3 now and enjoy both worlds of flying & building.....just a thought.... r.r.urban(at)worldnet.att.net on 01/20/2000 01:03:42 PM Please respond to rv-list(at)matronics.com Subject: RV-List: Re: RV3-List: RV3 Mode of Operation Comparison Wouldn't it be interesting to know if those that broke wings in the past would not break this NEW wing as well? This is no reflection on this new wing what-so-ever, but there will be those that find themselves outside the limits..... of even of this new wing. Bob Urban ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Evan&Megan Johnson wrote: > > --> RV3-List message posted by: "Evan&Megan Johnson" > > I recently had a conversation with Tom at Vans about this subject. I was > bummed about the cost of the new wing since I only have a couple of hundred > dollars into my kit. I was trying in vain to get him to tell me I could buy > just parts of the new wing kit (spar strips) and substitute them for the old > ones in my kit. My kit is very old #68....so I even have the thinner flat > bar for the spar strips. After mentioning that I felt compelled to buy the > new wing because I didn't want to die in this thing, he straightened me out. > In his opinion there is nothing at all wrong with even the oldest wing > design. As long as the pilot keeps within the G limits. As I am a very > conservative pilot and have no intention of ever doing any aerobatics, it > was agreed that the original wing design is more than sufficient. There are > a whole lot of these things flying presently with no problems at all. The > few that have come down have been reputed to be doing some pretty serious > maneuvers. While I am planning on doing the simple modifications per the > later plans, I am convinced that buying the new wing is not necessary. The > only really big advantage in my view is in resale value. I probably wont > ever sell it any way. > Evan.....skinning first wing > ----- Original Message ----- > From: Linzel G . Civ - 43CES/CECP <Gray.Linzel(at)pope.af.mil> > To: RV3-List Digest Server > Sent: Thursday, January 20, 2000 8:36 AM > Subject: RV3-List: RV3 Mode of Operation Comparison > > > --> RV3-List message posted by: "Linzel G . Civ - 43CES/CECP" > > > > > I am wondering how many RV3 builders are content to fly with the older > > unmodified wings? > > While generally not of competition form, it seems I can > comfortably/smoothly > > perform loops, rolls and most variations thereof without exceeding 160 MPH > > or the normal category G limits much less the utility category limits. > > The RV3 I built may have been one of the last ones shipped before the > > production hold. It's a fairly light, bare bones copy with a 160 lb > pilot. > > I think I remember hearing a statement made that no RV3's have had > > catastrophic wing problems while being flown by their builder? > > > > Gray > > (like the color of my unpainted RV3) > ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: Panel holes
Date: Jan 20, 2000
> The 8 panel is geting a bit crowded. What is the min. separation > between instr. that anyone has used successfully on the stock panel > and/or any other thicker upgrades? I just cut my holes and mounted my instruements. I used 2.5" on the engine instruments (Electronics International) which just happens to be the exact size of the case resulting in a zero clearance situation. Then on my larger holes I used about a 3.25" center to center spacing after checking that the cases would clear. You can see the cuts at http://home.pacifier.com/~randyl/pgPanel.htm. I've since mounted all my instruments and am working on my avionics rack. I'll try to get some updated pics up by this weekend. Regards, Randy Lervold RV-8, #80500, panel etc. ________________________________________________________________________________
Date: Jan 20, 2000
From: "jah" <jah(at)abraxis.com>
Subject: How I Designed My Panel...
Hi all, With all this panel talk on the list I thought I would offer my experience with creating the panel for my RV-8. I started with Panel Planner and then decided that Panel Planner really frustrated me. It does not follow Windows conventions and appears to me to be very sloppy. I see its use for nothing more than looking at pretty instruments on a rough layout of your panel. In order to design a real panel I believe you need something more precise. I purchased a CAD program called DesignCAD. It was cheep for its abilities. I think I paid $120 for it at CompUSA. It can handle all AutoCAD files (dxf, dwg) with ease and works logically like most people would like a CAD package to work. I started by drawing precise templates of the instruments like the altimeter with its knob cutout etc. I also made a center point mark (cross) at the center of each instrument hole. Rather than importing or drawing an exact replica of the RV-8 panel I measured the width of the panel and height of the panel at its center. I then drew a horizontal line in the CAD program representing the bottom of the panel and a center line extending vertical from the midpoint of the horizontal line. I used these lines to place my instruments; starting at the center of the panel and working out word towards the sides. After completing the panel layout in DesignCAD I printed the panel on my laser printer. Note that most laser printers have the same resolution for both horizontal and vertical planes. It is important that you use a printer with this type of resolution setting. When printing from DesignCAD you have several options. I choose to print the drawing at full scale (1.0) and also choose to tile the pages since my laser printer can only print 8.5" x 11" sized pages. I also choose to have DesignCAD print tick marks in the corners of the pages. This resulted in six pages with part of my panel on each page. Rather than use regular paper to print the panel I used transparency film. Once printed I used Scotch tape to tape all the pages together by aligning the tick marks in the corners of all the pages. Once I had the pages taped together I had a full scale drawing of my panel. Now that the design work was completed and the panel was printed at full size I made some reference lines on the aluminum panel. I found the exact center of the panel vertically and drew a line on it with a Sharpe. I also drew a horizontal line across the bottom just above the bend making sure that it was perpendicular to the vertical center line. I then placed my full scale printout on top of the panel by lining up the vertical and horizontal lines on both the panel and printout. Note that the printout was on transparency film so it is very easy to line things up. I then taped the panel in place and used a punch and hammer to mark the center of each instrument hole. Using the punch marks on the aluminum panel I drilled out the instrument holes as well as the other cutouts for the avionics and such. I found this method very easy and very precise. If anyone has questions please feel free to ask. I should have pictures of the panel and the process in a few days and can post them if anyone is interested. I will also post my panel template and instrument templates to whoever would like them. Jeff Hawkins Atlanta, Georgia RV-8 Fuselage Stuff ________________________________________________________________________________
Date: Jan 20, 2000
From: John Field <jfield(at)pressenter.com>
Subject: Re: MA-4SPA Carb for sale
I have a new MA-4SPA carb for sale. The price is $1,000. Reply off the list to jfield(at)pressenter.com John Field W12373 848th Ave. River Falls, WI 54022 715-425-7064 ________________________________________________________________________________
From: PILOT8127(at)aol.com
Date: Jan 20, 2000
Subject: Re: RV3-List: RV3 Mode of Operation Comparison
Hi RVers, I got two-cents worth. Remember this: "thou holdest the mighty wing-seperator, in thy HAND! While talking to my F-16E buddy (and local pilot) on this subject. He reminded me that ANY wing can fail. My three has the "modified" wing. I have put 6.5 G's on it during LEVEL flight. Avoid the rolling AND pulling manuvers. And, leave yourself an "OUT" if things get ugly...........: ) off the soap-box now, Gary (aka AJ) INDY RVs flyout-director (you only need one seat) ________________________________________________________________________________
Date: Jan 20, 2000
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: fuel line holes
several inches where the fuel line exits. "Stephen J. Soule" wrote: > > > It seems to me that the bulkhead fitting also lets you be a little less > fussy about where the fuel line exits the fuselage. As designed, the fuel > line has to come out and be precisely lined up with the fuel outlet on the > wing tank. By using a bulkhead fitting, you have more freedom about where > you locate the fitting because you are going to run a flexible line or a > solid line with a loop to the wing. > > BTW, how much space is there between the wing and the side of the fuselage. > I once had my wings on when I drilled the landing gear mounts, but I did not > make a note of the width of that space. > > Steve Soule > Huntington, Vermont RV-6A > > -----Original Message-----I would use either solid line with > a vibration loop or the aeroquip flex that > Vans has. I like the bulkhead method because it adds a solid > tie point. The flex > option allows the bent fittings ( 45 & 90 degree) to be > used. A little more > expensive but inthe large picture of building expenses- a > drop in the bucket... > ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)petroblend.com>
Subject: Re: RV3 Mode of Operation Comparison
Date: Jan 20, 2000
Long term listers will recall a conversation here regarding the "wing removal lever." Comments about being able to complete gentle aerobatics in your unmodified RV-3 are no different than doing acro in your family C-172. Will it do it? Absolutely. Is it smart? Absolutely not! What happens when you are pulling 3 'G's coming around that loop and you see a Canada goose up close and personal? I put 5 "Gs" on the meter in the panther and I was straight and level when it happened. The G vs stick force gradient for an RV is pretty flat. much flatter than your fathers 172 and tons flatter than your mothers Cherokee. Hence the chance of seeing a big number on the meter due to an inadvertant pull on the "wing removal lever" is much greater. Throw in the fact that you are operating near the limit already and we could have another article about homemade airplanes being deadly. I don't care how gray your hair is, or how much Viagra you use, in an RV EVERYONE is 21 yrs old and a fighter pilot!!! Do the right thing, modify the wing. Tailwinds, Doug Rozendaal dougr(at)petroblend.com www.petroblend.com/dougr ________________________________________________________________________________
Date: Jan 20, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Shielded wire for phones
> >Another question about headphone wiring. On one of Bob Nuckolls' drawings, >he shows the headphone jack wired w/ 2 conductor shielded wire with the >wires soldered to the tip and ring terminals and the shield bonded to the >ring conductor only at the audio panel termination. (i.e.. the shield is not >connected at the jack end) Look again. The shield is used to carry the signal ground from jack to the radio or intercom location. I bought a set of jacks that were already >prewired and the phone jack was wired with a single conductor shielded wire >with the shield soldered to the ring terminal. "Ring" terminal? are we talking mono or stereo headset? "Two conductor" jacks for microphones have tip, ring and sleeve or barrel terminals. The sleeve terminal is always signal ground. Mono headsets have only a tip terminal on their plug and would get the center conductor of a shielded feedline. The shield would go to the sleeve. If you have stereo headsets, the shield still goes to sleeve and a second wire under the shield would pick up the ring terminal. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Post-1st Flight Inspection
Date: Jan 20, 2000
> >Brian, > >Any tips, in hindsight, on tank sealing? I'm currently wrestling with >proseal myself. > >Larry Bowen >RV-8 tanks >Larry(at)BowenAero.com >http://BowenAero.com Larry, Yeah, USE LOTS OF IT! Ok, maybe it's not quite that simple, but just don't be afraid to use it. For some reason, the only leaking rivets I have had (this is the second one) have been on the stiffeners. Make a complete fillet of sealant around the entire flange of each stiffener as well as over every shop head. Build up fillets along every rib to skin junction and be extra thorough around the end ribs and nose reinforcement plates. No body is going to see your sealant work on the inside of the tank, so use the goop freely. I bought two full kits of sealant, and didn't even use up the first can. I think now that a full can should be used on the -8 tanks. You do have to be cautious on the rear baffle, as too much sealant will just make a mess of things and can make getting the tank back on the wing rather difficult. Make the sealant a very uniform thickness along the baffle flanges and after it's on, goop the corners real good. You only need a small patch of sealant under the Z brackets and only at each rivet hole, since these rivets are sealed anyway. Go with a thin film of sealant only, or it will move the brackets off the baffle face just enough to make the tank not sit down on the spar correctly. A little dab will do ya here. Hang in there. You'll do fine. Brian Denk RV8 N94BD 21 hours. ________________________________________________________________________________
Date: Jan 20, 2000
From: "Mike Wills" <willsm(at)spawar.navy.mil>
Subject: Re: RV3 Mode of Operation Comparison
> > I put 5 "Gs" on the meter in the panther and I was >straight and level when it happened. > >Tailwinds, >Doug Rozendaal >dougr(at)petroblend.com >www.petroblend.com/dougr Doug, 5G in straight and level flight?? Isnt that a sort of contradiction in terms?? Can we assume you mean straight and level in strong turbulence?? If so that must have been quite a bump. The first time that happens to me with my wife in the back seat will probably be the last time my wife is ever in the back seat!! Mike Wills RV4 engine installation (Mazda 13B) willsm(at)spawar.navy.mil ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: Scott McDaniels
Date: Jan 20, 2000
> Any of you folks up around Hillsboro know if Scott is fed up and has left > the list or is he just on vacation or something? The former. As he indicated in one of his last messages, he has left the list for now, and frankly, I can understand why. That long thread on "profit" was the way out of bounds and I think put him over the line. In principle this list is supposed to be for the exchange of RV-related information for the purpose of building or operating RVs. It is that, but it also becomes a forum for personal opinions on lots of things not necessarily RV-related, and frequently degrades from there. Frankly, some people are qualified to render judgments on various technical matters and others are not. On the list we have no way of knowing what each other's credentials are so everyone is an expert. There is a tendency for unqualified individuals to put forth information as fact that is simply bad information. I believe that, and all of the childish bickering, put him over the top. I live in the Portland area and talk with Scott fairly frequently (he's a member of our builder's group, the Home Wing VAF, and attends the local EAA breakfasts). I know for a fact both of these things bother him significantly. I believe that if one is to successfully tolerate this list one needs to have fairly thick skin, and also be willing to wade through the rhetoric to get to the factual information. I must admit, I've been tempted to leave the list myself. But then some really useful information gets exchanged and I stay up with it. Don't get me wrong, this list has been a huge resource for me through my 2+ years of building, but I too get very disappointed in the level of maturity and responsibility that sometimes gets displayed here. FWIW, Randy Lervold ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: fuel line holes
Date: Jan 20, 2000
> BTW, how much space is there between the wing and the side of the fuselage. > I once had my wings on when I drilled the landing gear mounts, but I did not > make a note of the width of that space. > > Steve Soule > Huntington, Vermont RV-6A About 3" from the fuse skin to the tank rib fore, around 2.5" aft end by spar. Subtract around .5" for tank rib flange overhang. Alex Peterson 6A ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: Post-1st Flight Inspection
Date: Jan 20, 2000
> 2. Pipe threads are hard to seal. I mounted my fuel flow transducer on the > firewall. A straight fitting was used on the inlet and a 90 elbow on the > exit. In order to get the elbow pointed forward, it was not fully tight. > Thread sealant was used on all pipe threads. Green stains were on the > transducer after the first flight, indicating a fuel leak. Last night I > removed the transducer & tighten the fitting. Fully tight, it was pointed > aft onto the firewall. I removed the fitting and retightened several times. > Each time the fitting turned more toward the front. With some serious > tightening, the fitting is facing forward and no leaks with the system > pressurized. Rick, what sort of thread sealant did you use? Also, I understand that there have been problems with cracks in the fuel transducer, so be very careful. High pressure fuel leaking from the firewall could be the big bummer. If you were progressively getting more rotation with each tightening, something was yielding. Alex Peterson Maple Grove, MN 6A ________________________________________________________________________________
From: JusCash(at)aol.com
Date: Jan 20, 2000
Subject: Re: Shielded wire for phones
Bob I just finished wiring my avionics stack. I'm using the PS Engineering PMA6000M audio selector panel with intercom and marker beacon. Their instruction's say to use two conductor shielded wire for the headphone jacks and three conductor shielded wire for the mic jacks. "All mic and headphone jacks must have insulating washer's, the shield must only be connected to the ground return wire only at the intercom connector." The shield is floating at the jack's. What would have happened if I had used the sleeve to ground the shield? Cash Copeland RV6 Oakland, Ca In a message dated 1/21/00 12:02:56 AM GMT Standard Time, nuckolls(at)aeroelectric.com writes: << "Ring" terminal? are we talking mono or stereo headset? "Two conductor" jacks for microphones have tip, ring and sleeve or barrel terminals. The sleeve terminal is always signal ground. Mono headsets have only a tip terminal on their plug and would get the center conductor of a shielded feedline. The shield would go to the sleeve. If you have stereo headsets, the shield still goes to sleeve and a second wire under the shield would pick up the ring terminal. >> ________________________________________________________________________________
Date: Jan 20, 2000
From: n3773 <n3773(at)mciworld.com>
Subject: common RV frequency, builders services directory
After reading about some upcoming SW trips it got me thinking about the idea of a common RV frequency, like 122.75 except different. It seems to me that the radio has 720 available, most airports use but a dozen. I know technically it's not legal, but hey, there's strength in numbers, right? Brian and I use 136.00 when flying as a flight since we're still quite the novices. Maybe some combination of the RV digits 3,4,6,8,9 could be found. At 10,000' I've spoken with pilots clear across the state of Oregon. If you've flown your unpainted plane yet you'll realize that another unpainted RV could be a few thousand feet away and out of sight. E-mail me off line if you'd like an updated copy of the RV Builders Services Directory. We have lodging in TX, AZ, CA, UT plus many other states and provinces(23 pages now). Maybe some NM builders (none so far) could enlist and get the chance to meet other builders/flyers. Kevin Lane N3773(at)mciworld.com ________________________________________________________________________________
Date: Jan 20, 2000
From: Thomas McIntyre <bogeybrother(at)earthlink.net>
Subject: spinner
If anyone out there has done any speed testing with and without a spinner I'd like to know if you were able to document any differences in speeds. Please contact me off-list. Thanks Tom RV3 ________________________________________________________________________________
From: A20driver(at)aol.com
Date: Jan 20, 2000
Subject: Re: spinner
Tom: The answer to your spinner question can be found on a tape by Mike Arnold when he researched and developed the AR-5 that holds the worlds record for its weight class, over 200 and something with a RotaX engine....The tape is called "Why it goes so fast" and can be had from The Arnold Co., 5960 S. Land Park Dr. 361,,Sacramento, CA, 95822....Cost ???....What he found out was the spinner didn't make one bit of difference on anything....engine temp, etc....He finally left it on because it made it look better....Regards, Jim Brown, NJ, 2-RV-3s and an RV-4 ________________________________________________________________________________
Date: Jan 20, 2000
From: Thomas McIntyre <bogeybrother(at)earthlink.net>
Subject: Re: spinner
Thanks Jim Petty much what I've been told also. Mike designed a F1 racer for a friend of mine and I've spoken with a number of times. He'd be the one to know. Happy FLying Tom A20driver(at)aol.com wrote: > > Tom: The answer to your spinner question can be found on a tape by Mike > Arnold when he researched and developed the AR-5 that holds the worlds record > for its weight class, over 200 and something with a RotaX engine....The tape > is called "Why it goes so fast" and can be had from The Arnold Co., 5960 S. > Land Park Dr. 361,,Sacramento, CA, 95822....Cost ???....What he found out was > the spinner didn't make one bit of difference on anything....engine temp, > etc....He finally left it on because it made it look better....Regards, Jim > Brown, NJ, 2-RV-3s and an RV-4 > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 21, 2000
Subject: Re: How I Designed My Panel...
In a message dated 1/20/00 1:08:59 PM Pacific Standard Time, jah(at)abraxis.com writes: << After completing the panel layout in DesignCAD I printed the panel on my laser printer. Note that most laser printers have the same resolution for both horizontal and vertical planes. It is important that you use a printer with this type of resolution setting. When printing from DesignCAD you have several options. I choose to print the drawing at full scale (1.0) and also choose to tile the pages since my laser printer can only print 8.5" x 11" sized pages. >> Would you like to buy a Houston Instruments DMP-51 Engineering 'D' size pen plotter with serial cable so you can print larger formats. It's yours for $250 plus shipping. I now have an HP Draftmaster and no longer need the Houston Instruments. -GV ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: Re: common RV frequency, builders services directory
Date: Jan 20, 2000
Fantastic idea...I don't think a special combination is necessary, just an arbitrary frequency that is not commonly used. Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit ----- Original Message ----- From: "n3773" <n3773(at)mciworld.com> Sent: Thursday, January 20, 2000 8:23 PM Subject: RV-List: common RV frequency, builders services directory > > After reading about some upcoming SW trips it got me thinking about the > idea of a common RV frequency, like 122.75 except different. It seems to > me that the radio has 720 available, most airports use but a dozen. I know > technically it's not legal, but hey, there's strength in numbers, right? > Brian and I use 136.00 when flying as a flight since we're still quite the > novices. Maybe some combination of the RV digits 3,4,6,8,9 could be found. > At 10,000' I've spoken with pilots clear across the state of Oregon. If > you've flown your unpainted plane yet you'll realize that another unpainted > RV could be a few thousand feet away and out of sight. > E-mail me off line if you'd like an updated copy of the RV Builders > Services Directory. We have lodging in TX, AZ, CA, UT plus many other > states and provinces(23 pages now). Maybe some NM builders (none so far) > could enlist and get the chance to meet other builders/flyers. > Kevin Lane N3773(at)mciworld.com > > ________________________________________________________________________________
Date: Jan 20, 2000
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: Condition Insp Checklist for RV-6A
> >Time has come for my first annual condition inspection. If anyone has >an inspection checklist for -6A with fixed pitch prop, I would >appreciate your sending it via email DIRECT. I am currently refining a >checklist intended for a -6 with cs prop. > >On the first day of inspection we found that the alternater housing >(Vans) and the alternator arm (ours) have been in contact with the lower >cowl and almost worn their way through...didn't notice it at last oil >change but it must have been there. Not the usual smiley face, just >craters! > >Will Cretsinger, Arlington, Texas >First annual at 152.7 hrs and 211 landings Will, Maybe the checklist below will be of some value or at least a place to start. Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 ************************* INSPECTION REPORT Type of Inspection __________________ OWNER: _________________________ DATE: _________ MAKE: _________ HOURS: _________ "N" #: _________ SER. #: _________ DESCRIPTION A. PROPELLER GROUP 1.______ Inspect spinner and back plate 2.______ Inspect blades for nicks and cracks 3.______ Check for grease and oil leaks 4.______ Lubricate propeller per lubrication chart 5.______ Check spinner mounting brackets 6.______ Check propeller mounting bolts and safety 7.______ Inspect hub parts for cracks and corrosion B. ENGINE GROUP CAUTION: ground mags before working on engine 1.______ Remove engine cowl 2.______ Clean and check cowling for cracks, distortion and loose or missing fasteners 3.______ Drain oil sump 4.______ Clean suction oil strainer at oil change 5.______ Clean pressure oil strainer or change full flow oil filter element 6.______ Check oil temp. sender for leaks and security 7.______ Check oil lines and fittings for leaks, chafing, security, dents and cracks 8.______ Clean and check oil radiator cooling fins 9.______ Fill engine with oil per lubrication chart 10._____ Clean engine 11._____ Check condition of spark plugs, adjust gap to:______ clean, test, rotate 12._____ Check ignition harness and insulators 13._____ Check magneto points for proper clearance maintain at .018 +- .006 14._____ Check magneto for oil seal leaks 15._____ Check breaker felt for proper lubrication 16._____ Check distributor block for cracks, burned areas or corrosion 17._____ Check magnetos to engine timing Left______ Right _______ 18._____ Remove air filter and clean 19._____ Drain carburetor and clean inlet line fuel strainer 20._____ Check condition of carburetor heat air door and box 21._____ Check intake seal for leaks and clamps for tightness 22._____ Clean fuel screens 23._____ Clean and check gasolator 24._____ Inspect condition of fuel lines 25._____ Check fuel system for leaks 26._____ Check electric fuel pump for operation 27._____ Check engine controls throttle, carb heat, mixture, and prop 28._____ Inspect exhaust stacks, connections, gaskets 29._____ Inspect heat exchange, baffles and shrouds 30._____ Check breather tube for obstructions and security 31._____ Check crankcase for cracks, leaks, security of bolts 32._____ Check engine mounts for cracks and loose mountings 33._____ Check all engine baffles 34._____ Check firewall seals 36._____ Check condition and tension of alternator and drive belt 36._____ Check condition of starter 37._____ Check fluid in brake reservoir 38._____ Lubricate all controls 39._____ Inspect engine for general condition, loose parts, chafing, proper safties and proper installation 40._____ Check condition of alternator 41._____ Check vacuum pump and lines 42._____ Compression check #1______ #2______ #3 ______ #4 ______ #5 ______ #6 ______ 43._____ Grease starter gear with moly 44._____ Reinstall engine cowl C. CABIN GROUP 1._____ Inspect canopy and windows 2._____ Check upholstery for tear 3._____ Check seats, seat belts, shoulder straps 4._____ Check trim operation 5._____ Check rudder pedals 6._____ Check control column, systems and connection 7._____ Check landing, nav, cabin, and instrument lights 8._____ Check instrument, lines and attachments 9._____ Check gyro operation, and electric turn and bank 10.____ Check or replace gyro air filter 11.____ Clean or replace vacuum regulator filter 12.____ Check altimeter 13.____ Check operation of fuel selector valve 14.____ Check operation of engine primer 15.____ Check condition of heater controls 16.____ Check condition and operation air vents 17.____ Check flap operation 18.____ Check fuel drains 19.____ Lubricate aileron, flap and elevator controls 20.____ Check general condition uder panel for loose wires, chafing, etc. 21.____ Check brake cylinders for operation and leaks D. FUSELAGE AND EMPENNAGE GROUP 1._____ Remove inspection plates and panels 2._____ Check battery box, battery and cables 3._____ Check electronic installations 4._____ Check bulkheads and stringers for damage 5._____ Check antenna mounts and wiring 6._____ Check fuel lines and valves 7._____ Check vertical fin and rudder surfaces 8._____ Check rudder horn and attachment 9._____ Check vertical fin attachments 10.____ Check rudder bolts for wear 11.____ Check horizonal stabilizer and elevators 12.____ Check horizonal stabilizer attachment 13.____ Check elevator horn 14.____ Check elevator bolts for wear 15.____ Check elevator bell cranks and controls and trim system 16.____ Lubricate all bearings as needed 17.____ Check general condition of skin 18.____ Check doors, latches and hinges 19.____ Check wiring for damage and security 20.____ Check cables for damage, security and operation 21.____ Check cabin heater and controls 22.____ Service hydraulic brake system 23.____ Check drain holes in rudder bottom and fuselage 23.____ Reinstall inspection plates and panels E. WING GROUP 1._____ Remove inspection plates and fairings 2._____ Check surfaces and tip for damage and loose rivets and condition of walkways 3._____ Check aileron mounts and attachments 4._____ Check aileron bellcrank and control tubes 5._____ Check flaps and attachment for damages 6._____ Check all wing attachment bolts 7._____ Check fuel tanks and lines for leaks and chafing 8._____ Check fuel tank vents 9._____ Check pitot 10._____ Reinstall inspection plates F. LANDING GEAR GROUP 1._____ Check nose gear travel and damper tightness 2._____ Check main gear attachments 3._____ Check tires for cuts and wear 4._____ Remove wheel, clean, and repack bearings COTTER PINS IN AXLES? 5._____ Check wheels for cracks, corrosion and broken bolts 6._____ Check tire pressure_____ 7._____ Check brake lining and disc 8._____ Check brake lines 9._____ Check tailwheel assembly for integrity and grease tailwheel G. OPERATIONAL INSPECTION 1._____ Check fuel pump and fuel tank selector 2._____ Check fuel pressure 3._____ Check oil pressure and temperature 4._____ Check alternator output 5._____ Check manifold pressure 6._____ Check alternate air 7._____ Check vacuum gauge 8._____ Check gyros for noise and roughness 9._____ Check Cabin heat operation 10.____ Check magneto switch operation 11.____ Check magneto RPM variation Left_____ Right_____ Run up rpm_______ 12.____ Check throttle and mixture operation 13.____ Check propeller smoothness 14.____ Check electronic equipment operation: fuel gauges, tach, engine instrumensts 15.____ Check ELT for operation and battery date 16.____ Check static rpms 17.____ Check idle rpms H. GENERAL 1._____ A.D.s complied with 2._____ Manufacturers service letters complied with 3._____ Registration, Airworthiness Cerfificate, Operating Limitations Signature_________________________ Certificate No.________________________ ________________________________________________________________________________
From: "Randall Henderson" <randallh(at)home.com>
Subject: Re: Palm GPS units
Date: Jan 20, 2000
> > Colours nice guys, but you have to havethe right type of screen [snip] Anyone know how that new Garmin 295 handheld rates for sunlight readable? Anyone have one yet? Randall Henderson, RV-6 N6R (in the paint shop) Portland, OR http://www.edt.com/homewing ________________________________________________________________________________
From: "Evan&Megan Johnson" <evmeg(at)snowcrest.net>
Subject: Re: RV3 Mode of Operation Comparison
Date: Jan 20, 2000
I appreciate all of the concern and the input on this subject. It is safe to say that all who contribute actually do care if another wing separates and we all know that it is almost impossible to free yourself from the craft at this point. I also feel compelled to point out that almost any aircraft can be pushed to the outside limits of its design if it flown in such a manner. Of course there will be the occasional Canada goose to screw with your world, but as with any other aircraft, you cant plan on every contingency. I have heard stories of such encounters putting down fighter jets designed for much more aggressive maneuvers than an RV. We all have to draw our own line based upon our own flying style. I actually do fly (and drive for that matter) in such a way as to be accused of being a little old lady by friends. If I never plan on doing even the mildest form of aerobatics, I would think that an airplane that was designed to be pushed pretty darn hard in this regard would have no problems at all. Remember, this is still supposed to be safe up to 6 G's! I am still planning on doing the wing modifications prior to the latest design. While I am sure that the new wing is superior to the one I am building, my own flying style does not seem to demand it. This is the precisely the kind of debate I was hoping to incite......if you have good reason to talk me or any other prospective builders out of the old design, lets hear it!.....Thanks in advance, you might be saving my life, Evan Message ----- From: Doug Rozendaal <dougr(at)petroblend.com> Sent: Thursday, January 20, 2000 3:25 PM Subject: Re: RV-List: RV3 Mode of Operation Comparison > > Long term listers will recall a conversation here regarding the "wing > removal lever." Comments about being able to complete gentle aerobatics in > your unmodified RV-3 are no different than doing acro in your family C-172. > Will it do it? Absolutely. Is it smart? Absolutely not! What happens when > you are pulling 3 'G's coming around that loop and you see a Canada goose up > close and personal? I put 5 "Gs" on the meter in the panther and I was > straight and level when it happened. > > The G vs stick force gradient for an RV is pretty flat. much flatter than > your fathers 172 and tons flatter than your mothers Cherokee. Hence the > chance of seeing a big number on the meter due to an inadvertant pull on the > "wing removal lever" is much greater. Throw in the fact that you are > operating near the limit already and we could have another article about > homemade airplanes being deadly. > > I don't care how gray your hair is, or how much Viagra you use, in an RV > EVERYONE is 21 yrs old and a fighter pilot!!! > > Do the right thing, modify the wing. > > Tailwinds, > Doug Rozendaal > dougr(at)petroblend.com > www.petroblend.com/dougr > > ________________________________________________________________________________
Date: Jan 20, 2000
From: George McNutt <gmcnutt(at)intergate.bc.ca>
Subject: Accesories & Instrument Panel
Trying to design for future maintainability, getting lazy in my old age. I am presently in the process of cutting and drilling holes in my instrument panel and have discovered some of the components are supplied with tiny attachment nuts and screws making future removal/replacement for repairs very difficult. For example, the electric trim switch and LED indicator units are supplied with number two screws and nuts, the ELT monitor is designed for #4 screws & nuts. As these components are not designed into the removable portion of my panel, and some clearances are tight, I can imagine myself trying to crawl under the panel in a few years and trying to start a #2 nut in the semi darkness. Heck I can hardly see the thing on the workbench today. Checking Aircraft Spruce & Wicks catalogs I find no plate-nuts or similar attachments smaller than #6 so I am thinking of making individual collars to fit behind the inst. panel and around the components, rivited on and with threaded holes for the screws. However before I go to all that trouble I thought I would ask for the wisdom of RV-Listers for any simpler solutions or ideas. George McNutt 6-A inst pnl Langley, B.C. ________________________________________________________________________________
Date: Jan 20, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: common RV frequency
Check the 2000 AOPA Airport Directory on page 1-30. There is a list of Navigation and Communication Frequencies. The CAF (Warbirds) uses several different frequencies from the list. The SoCAL Wing of Van's Air Force will come up on 122.75 when flying some where. If there is "traffic" on 122.75 (SoCAL WVAF Channel # 1), we will go to a predetermined frequency that has been allocated by the FCC to "flight test stations of aircraft manufacturers". On the way back from Oshkosh, Walt (RV-6A, N79WH) and Dwain (RV-6, N164DH) meet Wayne Handley on the SoCAL WVAF "private" channel. Walt took a picture of the "Turbo Raven" flying off his wing. The "Turbo Raven" photo is not on the web but Walt's and Dwain's RVs were/are RV's of the Week on Van's Web Page. I recommend that we not be "scuff laws" but "TRY" to stay within the frequncies given to us. In the U.S., the registration of our "Homebuilt" aircraft lists us as the manufacturer. This is a hint for picking a semi-"Private" frequency that MAY not get you in trouble with the FCC since the FAA considers you an aircraft manufacturer. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: "Rick Caldwell" <racaldwell(at)hotmail.com>
Subject: Re: Post-1st Flight Inspection
Date: Jan 21, 2000
Alex, I use SEALUBE, bought from ACS. Yea, I am concerned about the transducer splitting. I looked it over and all is well. If it splits, it'll ruin my day. Rick > > 2. Pipe threads are hard to seal. I mounted my fuel flow transducer on >the > > firewall. A straight fitting was used on the inlet and a 90 elbow on >the > > > exit. In order to get the elbow pointed forward, it was not fully >tight. > > > Thread sealant was used on all pipe threads. Green stains were on the > > transducer after the first flight, indicating a fuel leak. Last night I > > removed the transducer & tighten the fitting. Fully tight, it was >pointed > > > aft onto the firewall. I removed the fitting and retightened several >times. > > Each time the fitting turned more toward the front. With some serious > > tightening, the fitting is facing forward and no leaks with the system > > pressurized. > >Rick, what sort of thread sealant did you use? Also, I understand that >there have been problems with cracks in the fuel transducer, so be very >careful. High pressure fuel leaking from the firewall could be the big >bummer. If you were progressively getting more rotation with each >tightening, something was yielding. > >Alex Peterson >Maple Grove, MN 6A > > ________________________________________________________________________________
From: "William J. Oke" <Jim_Oke(at)mbnet.mb.ca>
"RV3-List Digest Server"
Subject: Re: RV3-List: RV3 Mode of Operation Comparison
Date: Jan 21, 2000
I fly an older RV-3 with the original 1/8 x 1 1/4 aluminum bar laminated spar. I purchased my kit in 1980 (hey, that's 20 years ago now !). I did the root rib reinforcements during construction but not the spar reinforcement. My reading of the RV-3 accident reports is that (1) there were often significant structural defects introduced into the accidnt aircraft during construction (center section bolts left out and so on) and (2) the pilots were often seen attempting manuevers of the high - speed low pass - sharp pull up type and not what normally would be considered aerobatics. So I am will probably not bother with a new wing and be content to simply avoid any agressive aerobatic or high-g maneuvers. In fact since my RV-3 is registered in Canada, there is an "aerbatics prohibited" placard on my panel which I can seek approval to remove but that is a lengthy engineering and flight test process that I have no intent of pursuing. The new wing would not make any differenence to this. Besides I am busy with -6a construction as well now ! Jim Oke Winnipeg, Canada RV-3, C-FIZM ----- Original Message ----- From: Linzel G . Civ - 43CES/CECP <Gray.Linzel(at)pope.af.mil> Sent: January 20, 2000 10:36 AM Subject: RV3-List: RV3 Mode of Operation Comparison > --> RV3-List message posted by: "Linzel G . Civ - 43CES/CECP" > > I am wondering how many RV3 builders are content to fly with the older > unmodified wings? > While generally not of competition form, it seems I can comfortably/smoothly > perform loops, rolls and most variations thereof without exceeding 160 MPH > or the normal category G limits much less the utility category limits. > The RV3 I built may have been one of the last ones shipped before the > production hold. It's a fairly light, bare bones copy with a 160 lb pilot. > I think I remember hearing a statement made that no RV3's have had > catastrophic wing problems while being flown by their builder? > > Gray > (like the color of my unpainted RV3) ________________________________________________________________________________
From: TColeE(at)aol.com
Date: Jan 21, 2000
Subject: Re: Inspection today
Today is the inspection from the FAA. Going to be a long day at the hanger which is right down the taxi way from the FSDO. and they are having there open house today from 10;00 to 2;00 If no one comes from 8 to 10 will be this afternoon after 2. Going to go eat there goodies from 10 to 2 making my presence known. and incourageing them to come on down to the hanger and give it the once over. and then put it all togather, and then , and then going to make my first flight with in the week. I hope Terry E. Cole N468TC ________________________________________________________________________________
From: "Greg Yotz" <gyachts(at)kans.com>
Subject: Re: Palm GPS units
Date: Jan 21, 2000
I have a Casio E-100, HP 420 and Compaq Aero 2100. The Compaq looks great outside because it's a reflective type LCD. The Casio and HP are both rear lighted type LCDs. The Compaq looks good in the daylight but isn't very good at night. The Casio looks good in daylight with a glare shield and looks great at night or in overcast skys. I think it would depend some on the type of cockpit you had and whether or not you plan on flying at night. If you have a bubble canopy and fly during the day 99% of the time I would buy the Compaq. If you fly at night or don't mind the glare shield then I would pick the Casio. Also depends if your going to use the PDA for other things. Inside the Casio looks great while the Compaq looks washed out. For business use the Casio is the winner hands down but I do use the Compaq too. My two cents worth.... Greg -----Original Message----- From: Graham Jones <gratech(at)a1.com.au> Date: Thursday, January 20, 2000 5:05 AM Subject: Re: RV-List: Palm GPS units > >Colours nice guys, but you have to havethe right type of screen. I was >looking at the E100 the other day and the HP Jornada as well. It's high >summer here in OZ and the day was around 31C (100+F) ie. REAL BRIGHT!. Took >the handhelds out side and couldn't read the screen at all. They just >turned black!. > >Took the mono Compaq Aero (?) and the Casio E15 (16 grey scales)outside and >they didn't change a bit...... Seems that the latest techno isn't so >great - except where you pay heaps for it like in the Garmin GNS430 etc. > >Graham Jones >(SUNNY!) Australia > >----- Original Message ----- >From: Greg Yotz <greg(at)controlvision.com> >To: >Sent: Wednesday, January 19, 2000 2:42 AM >Subject: Re: RV-List: Palm GPS units > > >> >> To bad the Fuel Manager didn't have sensors for real updates. >> Has anybody seen a Palm Pilot at night inside the cockpit? >> I like the looks of the Casio E-100 PDA. It looks good and is color. >> >> I still like the color GPS Moving map at <http://www.controlvision.com> >> >> Greg >> >> >> -----Original Message----- >> From: Shelby Smith <shelbyrv6a(at)mindspring.com> >> To: rv-list(at)matronics.com >> Date: Sunday, January 16, 2000 10:11 PM >> Subject: RV-List: Palm GPS units >> >> >> > >> >A while back there was a discussion on the Palm units. >> > >> >I found this website with more information. >> > >> >FYI only. I am not advertising for them, but they are getting my >attention. >> > >> >http://www.aspenleaf.com/palm/ >> >-- >> >Shelby Smith >> >shelbyrv6a(at)mindspring.com >> >RV6A - Skinning Fuselage - 200HP >> >N95EB - reserved >> > >> >---------- >> > >> > >> >> > > ________________________________________________________________________________
From: "Medema, Douglas K." <DMedema@physio-control.com>
Subject: Firewall questions
Date: Jan 21, 2000
Hi listers, Well, I managed to complete the assembly of the sliding part of my RV-6A sliding canopy!! You don't know what that means unless you've done it! I have decided to start working on my firewall and have some questions: 1) I'm tall and don't have the worlds smallest feet. As a result, I don't want the battery in the standard -6 position. After talking with the guys in Van's prototyping shop, I am planning to put my battery on the forward side of the firewall like in the RV-8. In fact, I bought the RV-8 battery box. I mocked up a battery in cardboard and it all seems to fit ok though a lot tighter than in an -8 which has a longer engine mount. Has anybody seen another -6 with the battery on the firewall? If I mount it to the far right side of the firewall, will it get in the way of anything coming off the engine? I know I'll affect the c.g. a bit, but I'm using an 0-320 with a wood prop, so it will help more than hurt. 2) I'd like to get a list of all the items that might normally go on the firewall. I know various people have put some of these items at other locations, but I just want to get a fairly complete idea of what has been put on firewalls by RVers: 1) gascolator 2) oil cooler 3) brake master cylinder 4) transducer holder for oil pressure/oil temperature/fuel pressure?? 5) cabin heat box/cabin heat selector 6) battery 7) master and starter solenoids 8) 3) I'm planning to use the Vetterman exhaust and from stuff in the archives, probably leaning towards two Robbins heatmuffs. I seem to recall seeing pictures from a plane that used two heat boxes, one to each muff, and ran the heat boxes with separate controls to both sides of the cockpit. Can anyone direct me towards those pictures? Does anyone have any comments about using two muffs with two heat boxes? I am not an active participant on the list, so I would appreciate getting copied directly to my email address with any comments on the above. dmedema@physio-control.com Thanks. Doug Medema RV-6A #21140, sliding part of sliding canopy finished!!! ________________________________________________________________________________
From: "Chat Daniel" <cdaniel(at)fnbbaldwin.com>
Subject: Re: Scott McDaniels
Date: Jan 21, 2000
FWIW also....... Several times I have had conversations with the folks at Vans and gotten advice that contradicted what I had heard from the listers. When I brought this to the attention of the Vans folks, I got the distinct impression that a lot of misinformation flows from the listers......basically just the same thing Randy is saying. So good advice for the listers would be.....listen to what others say but be careful of believing something that doesnt sound right or definitely check with Vans if it is critical. Chat Daniel RV8 N678RV(reserved) -----Original Message----- From: Randy Lervold <randyl(at)pacifier.com> Date: Thursday, January 20, 2000 8:05 PM Subject: Re: RV-List: Scott McDaniels > >> Any of you folks up around Hillsboro know if Scott is fed up and has left >> the list or is he just on vacation or something? > > >The former. As he indicated in one of his last messages, he has left the >list for now, and frankly, I can understand why. That long thread on >"profit" was the way out of bounds and I think put him over the line. > >In principle this list is supposed to be for the exchange of RV-related >information for the purpose of building or operating RVs. It is that, but it >also becomes a forum for personal opinions on lots of things not necessarily >RV-related, and frequently degrades from there. Frankly, some people are >qualified to render judgments on various technical matters and others are >not. On the list we have no way of knowing what each other's credentials are >so everyone is an expert. There is a tendency for unqualified individuals to >put forth information as fact that is simply bad information. I believe >that, and all of the childish bickering, put him over the top. I live in the >Portland area and talk with Scott fairly frequently (he's a member of our >builder's group, the Home Wing VAF, and attends the local EAA breakfasts). I >know for a fact both of these things bother him significantly. > >I believe that if one is to successfully tolerate this list one needs to >have fairly thick skin, and also be willing to wade through the rhetoric to >get to the factual information. I must admit, I've been tempted to leave the >list myself. But then some really useful information gets exchanged and I >stay up with it. Don't get me wrong, this list has been a huge resource for >me through my 2+ years of building, but I too get very disappointed in the >level of maturity and responsibility that sometimes gets displayed here. > >FWIW, >Randy Lervold > > ________________________________________________________________________________
Date: Jan 21, 2000
From: Mike Thompson <grobdriver(at)yahoo.com>
Subject: Re: Firewall questions
> I am not an active participant on the list, so I would appreciate > getting copied directly to my > email address with any comments on the above. Good questions, Doug! I hope the answers also find their way to the list by way of .cc! Mike Thompson Austin, TX -6 N140RV (Reserved) Wings Do Not Anchive Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: Kbalch1(at)aol.com
Date: Jan 21, 2000
Subject: MAC elevator trim servo
Well, I'm puzzled again. Seems to happen more frequently these days. I can't quite make sense of Drawing 5's depiction of the trim servo installation. The only way it makes sense to me at all is if my two E-602 Z brackets were mislabeled as to left and right. Even granting that, there's no way they'll fit on the E-616 cover plate without some serious trimming of the brackets. Of course, this is mentioned nowhere in the manual. What am I missing here? Does someone have any pictures of this install? Regards, Ken Balch Ashland, MA RV-8 #81125 left elevator & trim tab ________________________________________________________________________________
From: DWENSING(at)aol.com
Date: Jan 21, 2000
Subject: RMI micro Monitor
To the listers who are using the RMI micro monitor....... Should I use a separate switch for the back lighting or have the back lighting on whenever the unit is on? Thanks for your input. Dale Ensing 6A finishing the wiring Cary, Illinois ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 21, 2000
Subject: Re: Inspection today
In a message dated 1/21/00 6:25:15 AM Pacific Standard Time, TColeE(at)aol.com writes: << Today is the inspection from the FAA. Going to be a long day at the hanger which is right down the taxi way from the FSDO. and they are having there open house today from 10;00 to 2;00 If no one comes from 8 to 10 will be this afternoon after 2. Going to go eat there goodies from 10 to 2 making my presence known. and encouraging them to come on down to the hanger and give it the once over. and then put it all together, and then , and then going to make my first flight with in the week. I hope >> Great looking plane. I wanted to salute it ; ) -GV ________________________________________________________________________________
From: BumFlyer(at)aol.com
Date: Jan 21, 2000
Subject: SMALL NUTS
In a message dated 1/21/0 0:17:52, gmcnutt(at)intergate.bc.ca writes: << I am presently in the process of cutting and drilling holes in my instrument panel and have discovered some of the components are supplied with tiny attachment nuts and screws making future removal/replacement for repairs very difficult. For example, the electric trim switch and LED indicator units are supplied with number two screws and nuts, the ELT monitor is designed for #4 screws & nuts. As these components are not designed into the removable portion of my panel, and some clearances are tight, I can imagine myself trying to crawl under the panel in a few years and trying to start a #2 nut in the semi darkness. Heck I can hardly see the thing on the workbench today. Checking Aircraft Spruce & Wicks catalogs I find no plate-nuts or similar attachments smaller than #6 so I am thinking of making individual collars to fit behind the inst. panel and around the components, rivited on and with threaded holes for the screws. However before I go to all that trouble I thought I would ask for the wisdom of RV-Listers for any simpler solutions or ideas. George McNutt 6-A inst pnl Langley, B.C. >> I noted both these problems in my instalation. Couldn't come up with anything better at the time so have experienced lost nuts with both units. I think eventuallly I will go to some sort of adhesive mounting for these as they are both so light. Also thought in retrospect, should have used sheet metal screws, which should be more than adequate for these small lightweight things. Of course at the moment I am stuck with these large holes which are not conducive to sheet metal screws. D Walsh ________________________________________________________________________________
Date: Jan 21, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Electroair ignition
> >The actual load depends on several factors. To 'protect' the circuit use a >5 to 10 amp device. (Breaker, Fuse, EXP Bus, what ever...) > >Greg The running load for Jeff's ignition system is under 1 amp. He shows 18AWG wire to hook it up for voltage drop considerations . . . which are obviously very tiny. The system does have an inrush current on the order of 7-8 amps when you first turn it on. Given that it's an electronic ignition, it should be wired to the always hot side of the battery contactor . . . it needs to run even if the DC power master switch is OFF. Use a 22AWG fusible link to drive 18AWG feedwire to the ignition toggle switch. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
From: "Eric.J.Henson(at)chase.com
(Content Technologies SMTPRS 2.0.15) with SMTP id for" ; Fri, 21 Jan 2000 11:29:55.-0500(at)matronics.com
Date: Jan 21, 2000
Subject: Re: Firewall questions
I think Werner Berry has his battery in the engine compartment. Gary Sobek should know, or at least have his e-mail. Eric "Medema, Douglas K." <DMedema@physio-control.com> on 01/21/2000 10:30:04 AM Please respond to rv-list(at)matronics.com Subject: RV-List: Firewall questions Hi listers, Well, I managed to complete the assembly of the sliding part of my RV-6A sliding canopy!! You don't know what that means unless you've done it! I have decided to start working on my firewall and have some questions: 1) I'm tall and don't have the worlds smallest feet. As a result, I don't want the battery in the standard -6 position. After talking with the guys in Van's prototyping shop, I am planning to put my battery on the forward side of the firewall like in the RV-8. In fact, I bought the RV-8 battery box. I mocked up a battery in cardboard and it all seems to fit ok though a lot tighter than in an -8 which has a longer engine mount. Has anybody seen another -6 with the battery on the firewall? If I mount it to the far right side of the firewall, will it get in the way of anything coming off the engine? I know I'll affect the c.g. a bit, but I'm using an 0-320 with a wood prop, so it will help more than hurt. 2) I'd like to get a list of all the items that might normally go on the firewall. I know various people have put some of these items at other locations, but I just want to get a fairly complete idea of what has been put on firewalls by RVers: 1) gascolator 2) oil cooler 3) brake master cylinder 4) transducer holder for oil pressure/oil temperature/fuel pressure?? 5) cabin heat box/cabin heat selector 6) battery 7) master and starter solenoids 8) 3) I'm planning to use the Vetterman exhaust and from stuff in the archives, probably leaning towards two Robbins heatmuffs. I seem to recall seeing pictures from a plane that used two heat boxes, one to each muff, and ran the heat boxes with separate controls to both sides of the cockpit. Can anyone direct me towards those pictures? Does anyone have any comments about using two muffs with two heat boxes? I am not an active participant on the list, so I would appreciate getting copied directly to my email address with any comments on the above. dmedema@physio-control.com Thanks. Doug Medema RV-6A #21140, sliding part of sliding canopy finished!!! ________________________________________________________________________________
Date: Jan 21, 2000
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Plane needs a home
I no longer maintain the classified section of the "RV Journal" but I am making an exception due to the following circumstances. I received this note yesterday: "My good friend, Ernie Cleveland, recently passed away and left me with the responsibility of selling his beautiful RV-6. I spent several years helping him build it and would buy it myself if it weren't for the project in my garage. Here are the details: N339EC, RV-6 O-320AIA/150hp, Bernie Warnke Prop, 1100 hrs SMOH Completed in 1998, TTAF approx.100hrs Terra TX/RX and Transponder, Blind Encoder Lauritsen Interior ( Gray with boosters) Canopy cover and tie down kit Garmin GPS 195 GPSmap, ELT and New Peltor Headsets Flight instruments either new or Century reconditioned Light weight B&C Starter. New Alternator $50,000. Firm( now) will probably ask 60K in the Spring. Aircraft is registered to Ernie Cleveland ( Deceased) The airplane flys great. Cruise is about 175mph, tops out around 185-190. I think it has a little too much prop but it could be tweaked for a little more speed. Most of the testing time was flown with Ernie's 185lb frame aboard with my meager 235lbs in the left seat. CG was never a problem. She'll fly straight 'cause she was built straight. She'll also roll with the best of them." Jim Boyle, (847) 795-8185 BOYLEJR(at)prodigy.net You can see a photo of this beautiful RV-6 on the front page of "The RV Journal": http://home.HiWAAY.net/~sbuc/journal/ Let's see if we can find a home for this beautiful aircraft. If our plane ever ended up in similar circumstances, we would want our fellow RVer's to come to the aid of our friends and family. Sam Buchanan "The RV Journal" http://home.HiWAAY.net/~sbuc/journal ________________________________________________________________________________
From: "Wallace R. Penney" <wallyp(at)interlog.com>
Subject: RV3 Fuse Tank
Date: Jan 20, 2000
Gray wrote: I have a few hundred hours on my RV3 that I built from a kit a few years ago. I opted for the fuselage fuel tank with no fuel pumps to the O-320. The only problem is that the longitudinal fuel baffle inside the tank has become partially detached from its spot welds. I have a factory welded fuse tank in my RV-3. Although the tank baffle is still secure I did have one of the spot welds develop a tiny leak, ie just a trace of red dye on the exterior. The tank does bulge with the addition of 150 lb of fuel and this may be the cause of some spot welds letting go. In my case, I also noticed that the forward wall of the bulging tank could touch the stiffners on the firewall (rub marks on the paint showed they had been in contact). I had to file a bit off the stiffners and I also epoxied wear strips onto the tank just to make sure there was no more contact between the parent tank material and the firewall stiffners. Hope this helps. Wally.......flying RV-3, Toronto ________________________________________________________________________________
Date: Jan 21, 2000
From: chris marion <flyrv6(at)cinci.infi.net>
Subject: firewall jigging
Dear listers, I am trying to mount my rv6 firewall to the fuselage jig, I need to drill the engine mount holes for attachment to the jig. I cant seem to find the dimensions on the prints, can someone point me in the rite direction. also the two existing holes in the top left and right corners of the firewall, are these pre drilled engine mount holes or just tooling holes. I checked the archives and could find no solid answer. thanks chris marion rv6 jigging fuselage in cincinnati ohio ________________________________________________________________________________
Date: Jan 21, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Shielded wire for phones
> >Bob >I just finished wiring my avionics stack. I'm using the PS Engineering >PMA6000M audio selector panel with intercom and marker beacon. Their >instruction's say to use two conductor shielded wire for the headphone jacks >and three conductor shielded wire for the mic jacks. "All mic and headphone >jacks must have insulating washer's, the shield must only be connected to the >ground return wire only at the intercom connector." The shield is floating >at the jack's. > >What would have happened if I had used the sleeve to ground the shield? I've wired many airplanes using the shield as "ground" for the sleeve connection thus reducing the number of wires needed in the path between jack and audio system. The wiring PS Engineering is equally functional, just takes more wires. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
Date: Jan 21, 2000
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: RMI micro Monitor
DWENSING(at)aol.com wrote: > > > To the listers who are using the RMI micro monitor....... > > Should I use a separate switch for the back lighting or have the back > lighting on whenever the unit is on? Thanks for your input. > Dale Ensing > 6A finishing the wiring > Cary, Illinois I connected the backlighting to the nav light circuit and have been pleased with the display in all lighting situations. Sam Buchanan "The RV Journal" http://home/hiwaay.net/~sbuc/journal ________________________________________________________________________________
Date: Jan 21, 2000
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Accesories & Instrument Panel
George McNutt wrote: > > > Trying to design for future maintainability, getting lazy in my old age. > > I am presently in the process of cutting and drilling holes in my > instrument panel and have discovered some of the components are supplied > with tiny attachment nuts and screws making future removal/replacement > for repairs very difficult. > > For example, the electric trim switch and LED indicator units are > supplied with number two screws and nuts, the ELT monitor is designed > for #4 screws & nuts. > > As these components are not designed into the removable portion of my > panel, and some clearances are tight, I can imagine myself trying to > crawl under the panel in a few years and trying to start a #2 nut in the > semi darkness. Heck I can hardly see the thing on the workbench today. > > Checking Aircraft Spruce & Wicks catalogs I find no plate-nuts or > similar attachments smaller than #6 so I am thinking of making > individual collars to fit behind the inst. panel and around the > components, rivited on and with threaded holes for the screws. > > However before I go to all that trouble I thought I would ask for the > wisdom of RV-Listers for any simpler solutions or ideas. > > George McNutt > 6-A inst pnl > Langley, B.C. Those of us who still have some R/C plane stuff lying around have a good solution to the problem of mounting very lightweight items such as the ELT monitor. The little sheetmetal screws we used to mount the servos in our models are just the right size (#2?) for attaching these small items to the panel. Drill the holes a little undersize and thread the screw directly into the panel. I haven't had any problems with the screws backing out. Sam Buchanan "The RV Journal" http://home.hiwaay.net/~sbuc/journal ________________________________________________________________________________
Date: Jan 21, 2000
From: Jim Cimino <jcimino(at)epix.net>
Subject: Governor Control question
Is anyone using the a Hartzell prop governor? What did you use for a cable mounting bracket? Jim Cimino RV-8 sn 80039 N7TL Reserved http://www.geocities.com/MotorCity/5771 (570)842-4057 N.E. Pennsylvania ________________________________________________________________________________
From: "Joe Wiza" <planejoe(at)ewol.com>
Subject: RV4, F-482
Date: Jan 21, 2000
Friend of mine bilding an RV4 can't find any info on PN F-482 left and right. Does anyone know where they go or better print #. TU planejoe(at)ewol.com ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Jan 21, 2000
Subject: Re: firewall jigging
Chris: I'm no expert but when I mounted my -6 firewall to the fuselage jig I decided not to drill any engine mount holes until I had the actual mount. Instead I used 1/4 in. lag screws through those two holes in the top corners (that I believe are supposed to match the engine mount) to attach the top ( its really on the bottom in the jig). I then made two clips of 0.063 X 1.0 in scrap al. that hooked over the edge of the firewall bottom angle and used those to secure the bottom of the firewall at the top of the jig uprights. These and some wooden spacers between the jig uprights and the firewall allowed me to adjust and hold the position of the firewall quite accurately until I got to fitting the forward bottom skin. By that time the structure was stiff enough that I could remove the clips without any problem. Hope this helps. ________________________________________________________________________________
From: "Bryan E. Files" <bfiles(at)corecom.net>
Subject: Palm Pilot
Date: Jan 21, 2000
Could any of you email me the location of any places that have Palm Pilot weight and balance and GPS software. Thanks in advance. Bryan ________________________________________________________________________________
Date: Jan 21, 2000
From: Bill VonDane <bvondane(at)atmel.com>
Subject: Palm Pilot
Here is the URL that was posted the other day: http://www.aspenleaf.com/palm/ -Bill Von Dane - Colorado Springs, CO RV-8A N912V res., waiting for wings http://vondane.tripod.com ________________________________________________________________________________
Date: Jan 21, 2000
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Wing root fairings questions
Do the wing root fairings normally need to be re-trimmed? Mine don't look like they fit. How close should the aluminum fairing be to the fuselage? That is, how much crush should the rubber strip be under? How do I drill for screws without hitting something such as rivet or worse, gas tank? Hal Kempthorne - SJC RV6a N7HK at SCK Hangar K3 Debonair N6134V for sale ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: Shielded wire for phones
Date: Jan 21, 2000
It is my understanding that only one end of the shielding should be grounded. Sometimes with both ends grounded, you get a ground loop and that might generate a hum. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Robert L. Nuckolls, III <nuckolls(at)aeroelectric.com> Date: Friday, January 21, 2000 11:31 AM Subject: Re: RV-List: Shielded wire for phones > >> >>Bob >>I just finished wiring my avionics stack. I'm using the PS Engineering >>PMA6000M audio selector panel with intercom and marker beacon. Their >>instruction's say to use two conductor shielded wire for the headphone jacks >>and three conductor shielded wire for the mic jacks. "All mic and headphone >>jacks must have insulating washer's, the shield must only be connected to >the >>ground return wire only at the intercom connector." The shield is floating >>at the jack's. >> >>What would have happened if I had used the sleeve to ground the shield? > > I've wired many airplanes using the shield as "ground" for the > sleeve connection thus reducing the number of wires needed in > the path between jack and audio system. The wiring PS Engineering > is equally functional, just takes more wires. > > > Bob . . . > > http://www.aeroelectric.com > > ________________________________________________________________________________
Date: Jan 21, 2000
From: Bill VonDane <bvondane(at)atmel.com>
Subject: RV's at Meadowlake Airport, 00V, in Peyton Colorado...
Hello All... I don't wish to get too off topic here, but all the talk lately about places to fly to spurred me to tell you all about our little airport... EAA Chapter 72 - http://eaa72.tripod.com is based at Meadowlake Airport - 00V, in Peyton, CO, just 14nm (26km) NE of Colorado Springs, at a field elevation of 6874 ft. We have more than 6 flying RV's, and more than 8 under construction at this time... I have added a page to my web site with information about the RV's and RV builders at our airport, and encourage you to take a look... http://vondane.tripod.com/colorv/ We try to have a little cook-out / get together on the Saturday after the 3rd Tuesday of each month, which just happens to be tomorrow for January. We'll be there from 9:00am till 1:00pm, and probably longer... If you in the neighborhood, drop in, say hey, and have a burger! I understand we're gonna have a few Russian aircraft visiting us tomorrow... On your way in, just let us know your inbound for an EAA burger, and we'll help you get to the right hanger... Thanks... -Bill Von Dane - Colorado Springs, CO RV-8A N912V res., waiting for wings http://vondane.tripod.com ________________________________________________________________________________
From: "Robert Hughes" <hawk(at)digisys.net>
Subject: Taildraggers
Date: Jan 21, 2000
At the risk of walking into the frag pattern again, I thought that the following note from Budd Davisson in the context of someone choosing between the 6 and 6A might be of interest to some. Hawkeye Hughes __________________ The RV series is in the top 10% of tailwheel airplanes in terms of docility and handling, which is to say, it's hard to justify adding a nose gear to a beautiful design. After over 28 years and 3000-4000 hours in the pattern doing nothing but teaching landings in Pitts Specials I can categorically say that the hardest problem I encounter is overcoming the BS about tailwheels each pilot carries around in his head. It generally takes no more than 2.5 hours to get them so they can keep the airplane between the white lines. They may not be pretty but they are safe. Getting them to fly a good approach is another matter altogether. If any tailwheel airplane is put on the ground straight, with no drift it will track more or less straight ahead with minor meandering when it slows down. This even applies to supposedly squirrely little buggers like the Pitts. Put any tailwheel airplane on crooked and it'll make you work. However, in just any airplane all it takes a careful understanding of what it is you're trying to accomplish to sort things out. If the nose swerves left (for example) your first concern is NOT getting it back straight with the runway. Your first concern is stopping the turn. Your second concern is bringing it back parallel. If you leave the rudder in long enough to bring it back to center, you have to answer that first foot with the other foot and you wind up dancing. On a reactive airplane, leaving the rudder in that long is setting the stage for a super-swerve. In 28 years I've never seen a Pitts ground looped, but I've seen dozens of them leave the runway on the third, and always final, swerve. All of this is a direct result of pilot action, not airplane action. Few modern taildraggers (read that as after the mid-30's) are natural ground loopers. That's just part of the tailwheel BS floating around. The key is understanding that getting the rudder off is almost as important as getting it on. The amount of time it takes to get your foot off the rudder is critical because the airplane feels as if it is getting half the total rudder deflection for the duration of the time it takes to get it out. The result of slowly "walking" the rudder is that you always have too much in. The instant any movement is noted in the direction of the down foot, the rudder should be removed. Treat the rudder like the hot water in the shower: turn the hot water on and the instant you feel it getting warm, turn it off. Much of the above effect is masked in slow reacting airplanes like Champs, but the effect is there nonetheless. Tailwheels are the subject of more old wive's tales and misunderstanding than just about any part of aviation. Yes, they require a little more skill and a little more training, but only a little. Also the training has to be of the right sort. Being able to do it is not the same as understanding it and the lack of understanding is why so many tailwheel airplanes get needlessly bent. Also, most of the training for tailwheel transition is getting a pilot to do what they were supposed to be able to do as students: hold a correct speed, coordinate, land with no drift, hold landing attitude and keep the tail straight behind the nose Sorry! Didn't mean to ramble on, but this is one of my hot buttons (obviously). Budd Davisson Plus 5 SportAERO ________________________________________________________________________________
From: Larygagnon(at)aol.com
Date: Jan 21, 2000
Subject: Re: SMALL NUTS
I've had success with Riv-nuts as small as 4/40 in light duty applications. They set like a rivet and give you a threaded hole for attachment. I used them on the interior console and instrument panel on my Kitfox and they have held up well. The kit I have has applicators for 4/40, 6/32.8/32, 10/32 and 1/4x20. Contact me off line if you need a source but they should be available locally. Larry Gagnon Kitfox 4/912 N102LG RV-6 Wings N6LG reserved ________________________________________________________________________________
From: "Stan Blanton" <stanb(at)door.net>
Subject: Re: Wing root fairings questions
Date: Jan 21, 2000
>snip >Do the wing root fairings normally need to be re-trimmed Yes, I had to trim mine quite a bit. snip >How close should the aluminum fairing be to the fuselage? That is, how >much crush should the rubber strip be under? > I set the gap at 3/16 with a piece of scrap bar stock as a spacer for a marking pen. >How do I drill for screws without hitting something such as rivet or worse, >gas tank? > The screws go thru the root rivet flange that faces inboard. Up front they go through the tank rib flange. Be sure you skip over the spar and its flanges. I drew an offset line that showed me how much to measure back after I had placed the fairing in place. Stan Blanton RV-6 stanb(at)door.net ________________________________________________________________________________
Subject: Re: Wing root fairings questions
Date: Jan 21, 2000
From: Larry Pardue <n5lp(at)carlsbad.net>
> >Do the wing root fairings normally need to be re-trimmed? Mine don't look >like they fit. Mine needed to be trimmed a lot. > >How close should the aluminum fairing be to the fuselage? That is, how >much crush should the rubber strip be under? Enough to make the weather strip have a nice curve up to meet the fuselage? Do tests. > >How do I drill for screws without hitting something such as rivet or worse, >gas tank? > > Measure back from the fuselage at each hole location then transfer that measurement to the fairing strip when it is in position. My methods only. Larry Pardue Carlsbad, NM RV-6 N441LP http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Breaker/switch orientation
Date: Jan 21, 2000
Electrical gurus, I have now arrived at my final panel layout (RV-8) and cut all of the holes, so I'm committed. The bottom of the panel features a row of Potter-Brumfield W23 series breakers and W31 series switch/breakers for most major functions. These will have their input terminals connected with a piece of copper strip for low voltage loss and good mechanical integrity... very standard practice. The problem however is that in using a combination of the pullable breakers and switch/breakers I find that the two terminals on each style have opposite functions. On the breakers the top terminal is labeled "line" and the bottom terminal "load". The switch/breakers are labeled in an opposite manner. Needless to say it would be far simpler to simply run my copper bus strip across the top, but then the switch/breakers would be then be wired in opposite fashion t thier labeling. My question is this: does it matter? I don't know what's inside of there, so if anyone has a clue why those switch/breakers couldn't be used in an opposite manner I'd appreciate knowing about it. Electric Bob? BTW, my layout can be seen at http://home.pacifier.com/~randyl/pgPanel.htm Thanks, Randy Lervold RV-8, #80500, panel, canopy skirt (again!) www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Jan 21, 2000
Subject: Re: Palm Pilot
http://www.aircalc.com/ heres another Chris Wilcox F-1 Rocket ________________________________________________________________________________
From: "Bill Shook" <skydiven(at)bellsouth.net>
Subject: Re: Taildraggers
Date: Jan 21, 2000
Dammit dammit dammit.....now that you've let the cat out of the bag, HOW are taildragger pilots supposed to claim superiority over 'lessor trained' pilots? Stop telling people it's no big deal! Taildraggers are vicious, pilot eating machines..... That's what I tell everyone when I tell them I was tail dragger signed off before I even took the written private pilot exam. You should have seen the look on MR. FAA's face when I showed him my medical and student solo endorsements during a ramp check as I climbed out of the Decathlon. :) You learned to fly in cessna 150's and transitioned to taildragger BEFORE getting a license? (he asked)...... I was bored and needed a challenge.....are we done now? (I responded). Bill ----- Original Message ----- From: "Robert Hughes" <hawk(at)digisys.net> Sent: Friday, January 21, 2000 2:45 PM Subject: RV-List: Taildraggers > > At the risk of walking into the frag pattern again, I thought that the following > note from Budd Davisson in the context of someone choosing between the 6 and 6A > might be of interest to some. > > Hawkeye Hughes > > __________________ > The RV series is in the top 10% of tailwheel airplanes in terms of > docility and handling, which is to say, it's hard to justify adding a > nose gear to a beautiful design. > > After over 28 years and 3000-4000 hours in the pattern doing nothing > but teaching landings in Pitts Specials I can categorically say that the > hardest problem I encounter is overcoming the BS about tailwheels each > pilot carries around in his head. It generally takes no more than 2.5 > hours to get them so they can keep the airplane between the white lines. > They may not be pretty but they are safe. Getting them to fly a good > approach is another matter altogether. If any tailwheel airplane is put > on the ground straight, with no drift it will track more or less > straight ahead with minor meandering when it slows down. This even > applies to supposedly squirrely little buggers like the Pitts. Put any > tailwheel airplane on crooked and it'll make you work. However, in just > any airplane all it takes a careful understanding of what it is you're > trying to accomplish to sort things out. > > If the nose swerves left (for example) your first concern is NOT getting > it back straight with the runway. Your first concern is stopping the > turn. Your second concern is bringing it back parallel. If you leave > the rudder in long enough to bring it back to center, you have to answer > that first foot with the other foot and you wind up dancing. On a > reactive airplane, leaving the rudder in that long is setting the stage > for a super-swerve. In 28 years I've never seen a Pitts ground looped, > but I've seen dozens of them leave the runway on the third, and always > final, swerve. All of this is a direct result of pilot action, not > airplane action. Few modern taildraggers (read that as after the > mid-30's) are natural ground loopers. That's just part of the tailwheel > BS floating around. > > The key is understanding that getting the rudder off is almost as > important as getting it on. The amount of time it takes to get your foot > off the rudder is critical because the airplane feels as if it is > getting half the total rudder deflection for the duration of the time it > takes to get it out. The result of slowly "walking" the rudder is that > you always have too much in. The instant any movement is noted in the > direction of the down foot, the rudder should be removed. Treat the > rudder like the hot water in the shower: turn the hot water on and the > instant you feel it getting warm, turn it off. > > Much of the above effect is masked in slow reacting airplanes like > Champs, but the effect is there nonetheless. > > Tailwheels are the subject of more old wive's tales and misunderstanding > than just about any part of aviation. Yes, they require a little more > skill and a little more training, but only a little. Also the training > has to be of the right sort. Being able to do it is not the same as > understanding it and the lack of understanding is why so many tailwheel > airplanes get needlessly bent. Also, most of the training for tailwheel > transition is getting a pilot to do what they were supposed to be able > to do as students: hold a correct speed, coordinate, land with no > drift, hold landing attitude and keep the tail straight behind the nose > > Sorry! Didn't mean to ramble on, but this is one of my hot buttons > (obviously). > > Budd Davisson > Plus 5 SportAERO > > ________________________________________________________________________________
Date: Jan 21, 2000
From: Ted Gauthier <blunist(at)flash.net>
Subject: Re: MAC elevator trim servo
The brackets that were sent to me were mislabeled and I had a lot of trimming to do. I have some great close up photo's of this on my web site: http://www.flash.net/~blunist/ Ted Gauthier blunist(at)flash.net Pontiac, Mich Waiting for RV-6 wing kit Kbalch1(at)aol.com wrote: > > Well, I'm puzzled again. Seems to happen more frequently these days. > > I can't quite make sense of Drawing 5's depiction of the trim servo > installation. The only way it makes sense to me at all is if my two E-602 Z > brackets were mislabeled as to left and right. Even granting that, there's > no way they'll fit on the E-616 cover plate without some serious trimming of > the brackets. Of course, this is mentioned nowhere in the manual. > > What am I missing here? Does someone have any pictures of this install? > > Regards, > Ken Balch > Ashland, MA > RV-8 #81125 > left elevator & trim tab > ________________________________________________________________________________
From: RV6captain(at)aol.com
Date: Jan 21, 2000
Subject: Harmon Rocket Information
Does anyone have any information on a Harmon Rocket website or somewhere that I can get some information on their quickbuild kits. Thanks, Eli Lewis Venice, FL RV-6 ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Jan 21, 2000
Subject: Re: Harmon Rocket Information
In a message dated 1/21/2000 4:40:28 PM Central Standard Time, RV6captain(at)aol.com writes: << Does anyone have any information on a Harmon Rocket website or somewhere that I can get some information on their quickbuild kits. Thanks, Eli Lewis Venice, FL RV-6 >> www.teamrocketaircraft.com Chris Wilcox F-1 Rocket builder ________________________________________________________________________________
From: "bobdz" <bobdz(at)email.msn.com>
Subject: Re: Harmon Rocket Information
Date: Jan 21, 2000
> > Does anyone have any information on a Harmon Rocket website or somewhere that I believe it is www.teamrocketaircraft.com ________________________________________________________________________________
From: "Charles Zaloom" <czaloom(at)worldnet.att.net>
Subject: Re: Taildraggers
Date: Jan 21, 2000
Now this really is out of hand! Next someone is going to say that it takes more time to learn how to use an approach-certified GPS than it does to "master" the tailwheel (which is about right). I'm all for painting "conventional" airplanes into the space reserved for GeeBee racers and sailing in the Bermuda Triangle. What else will separate us from the inferior biomasses that checked "the other" box on the kit order form? ----- Original Message ----- From: Bill Shook <skydiven(at)bellsouth.net> Sent: Friday, January 21, 2000 4:40 PM Subject: Re: RV-List: Taildraggers > > Dammit dammit dammit.....now that you've let the cat out of the bag, HOW > are taildragger pilots supposed to claim superiority over 'lessor trained' > pilots? Stop telling people it's no big deal! Taildraggers are vicious, > pilot eating machines..... That's what I tell everyone when I tell them I > was tail dragger signed off before I even took the written private pilot > exam. You should have seen the look on MR. FAA's face when I showed him my > medical and student solo endorsements during a ramp check as I climbed out > of the Decathlon. :) You learned to fly in cessna 150's and transitioned > to taildragger BEFORE getting a license? (he asked)...... I was bored and > needed a challenge.....are we done now? (I responded). > > Bill > > > ----- Original Message ----- > From: "Robert Hughes" <hawk(at)digisys.net> > To: "RV-List" > Sent: Friday, January 21, 2000 2:45 PM > Subject: RV-List: Taildraggers > > > > > > At the risk of walking into the frag pattern again, I thought that the > following > > note from Budd Davisson in the context of someone choosing between the 6 > and 6A > > might be of interest to some. > > > > Hawkeye Hughes > > > > __________________ > > The RV series is in the top 10% of tailwheel airplanes in terms of > > docility and handling, which is to say, it's hard to justify adding a > > nose gear to a beautiful design. > > > > After over 28 years and 3000-4000 hours in the pattern doing nothing > > but teaching landings in Pitts Specials I can categorically say that the > > hardest problem I encounter is overcoming the BS about tailwheels each > > pilot carries around in his head. It generally takes no more than 2.5 > > hours to get them so they can keep the airplane between the white lines. > > They may not be pretty but they are safe. Getting them to fly a good > > approach is another matter altogether. If any tailwheel airplane is put > > on the ground straight, with no drift it will track more or less > > straight ahead with minor meandering when it slows down. This even > > applies to supposedly squirrely little buggers like the Pitts. Put any > > tailwheel airplane on crooked and it'll make you work. However, in just > > any airplane all it takes a careful understanding of what it is you're > > trying to accomplish to sort things out. > > > > If the nose swerves left (for example) your first concern is NOT getting > > it back straight with the runway. Your first concern is stopping the > > turn. Your second concern is bringing it back parallel. If you leave > > the rudder in long enough to bring it back to center, you have to answer > > that first foot with the other foot and you wind up dancing. On a > > reactive airplane, leaving the rudder in that long is setting the stage > > for a super-swerve. In 28 years I've never seen a Pitts ground looped, > > but I've seen dozens of them leave the runway on the third, and always > > final, swerve. All of this is a direct result of pilot action, not > > airplane action. Few modern taildraggers (read that as after the > > mid-30's) are natural ground loopers. That's just part of the tailwheel > > BS floating around. > > > > The key is understanding that getting the rudder off is almost as > > important as getting it on. The amount of time it takes to get your foot > > off the rudder is critical because the airplane feels as if it is > > getting half the total rudder deflection for the duration of the time it > > takes to get it out. The result of slowly "walking" the rudder is that > > you always have too much in. The instant any movement is noted in the > > direction of the down foot, the rudder should be removed. Treat the > > rudder like the hot water in the shower: turn the hot water on and the > > instant you feel it getting warm, turn it off. > > > > Much of the above effect is masked in slow reacting airplanes like > > Champs, but the effect is there nonetheless. > > > > Tailwheels are the subject of more old wive's tales and misunderstanding > > than just about any part of aviation. Yes, they require a little more > > skill and a little more training, but only a little. Also the training > > has to be of the right sort. Being able to do it is not the same as > > understanding it and the lack of understanding is why so many tailwheel > > airplanes get needlessly bent. Also, most of the training for tailwheel > > transition is getting a pilot to do what they were supposed to be able > > to do as students: hold a correct speed, coordinate, land with no > > drift, hold landing attitude and keep the tail straight behind the nose > > > > Sorry! Didn't mean to ramble on, but this is one of my hot buttons > > (obviously). > > > > Budd Davisson > > Plus 5 SportAERO > > > > > > ________________________________________________________________________________
Date: Jan 21, 2000
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: Wing root fairings questions
Hal, The fairings do need to be trimmed to fit. I fit mine to where there was very slight contact of the rubber molding to the side of the fuselage. Did the same on Charlie Tyrell's 6A. Something we did on Charlie's 6A that you might want to consider. I think it turned out nice. However----this is a departure from the plans and, as a tech counselor, I shouldn't really promote that. We carried the line of fastners in a straight line. In other words, we matched the row of holes to those of the fuel tanks. The holes/nutplates in the wing portion were in the skin area as opposed to being located in the main, root rib. This gives you the same edge distance for the screw holes and a nice straight line down the fairing. We used #6 countersunk screws. As I said, this is not "per plans" and may not have the blessing of Van's. For locating holes for blind drilling in this area (and for any other area), I mark the hole location and lay the corner of a 12" rule on the location. I then draw a line 8 inches or so long and mark the line at the 5 or 6 inch location (with a notation at the mark of the distance.) Then, lay the fairing on the wing, line up the ruler with the line and the index mark and put a dot at the corner of the rule. You can use this method on pre-drilled holes, as well. I think this is just as accurate as using a hole finder when you consider that a #40 hole will eventually be upsized for a #6 or #8 screw. The thickness of a hole finder seems to me like it might mess up a nice tight fit of the fairing to the wing. Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 > >Do the wing root fairings normally need to be re-trimmed? Mine don't look >like they fit. > >How close should the aluminum fairing be to the fuselage? That is, how >much crush should the rubber strip be under? > >How do I drill for screws without hitting something such as rivet or worse, >gas tank? > > >Hal Kempthorne - SJC >RV6a N7HK at SCK Hangar K3 >Debonair N6134V for sale ________________________________________________________________________________
Date: Jan 21, 2000
From: Larry Olson <lolson(at)doitnow.com>
Subject: Re: firewall jigging
Chris, I used a drywall screw thru the two existing holes, then clamped the two bottom spots. I don't think you want to drill the engine mount holes until you have the mount to use as a template. Larry > >Dear listers, > I am trying to mount my rv6 firewall to the fuselage jig, ________________________________________________________________________________
From: "Tim Lewis" <timrv6a(at)earthlink.net>
Date: Jan 21, 2000
Subject: Re: Wing root fairings questions
> Do the wing root fairings normally need to be re-trimmed? Mine don't look > like they fit. I had to trim mine. > How do I drill for screws without hitting something such as rivet or > worse, gas tank? As I recall, I drew a reference line on the wing a few inches outboard from the fuselage. Then I located where I wanted each hole drilled without the metal fairing being in place. I drew a line from each desired hole location back thru (and perpendicular to) the reference line. I noted the distance between the reference line and the desired hole location. Then I put the metal fairing in place, used the lines to locate the desired hole location, and drilled thru the fairing and the wing. Worked fine. Tim. ****** Tim Lewis -- Springfield VA RV-6A N47TD - First Flight 18 Dec 99 TimRV6A(at)earthlink.net http://www.geocities.com/timrv6a ________________________________________________________________________________
Date: Jan 21, 2000
From: wayne bonesteel <wayneb(at)oakweb.com>
Subject: Re: RV4, F-482
Joe the F-482's are the rear seat bulkhead re-inforcements get service bulletin 97-5-1 from Vans. I were no drawings on this for my plane (#4148) I made them and installed them myself. I think one of the earlier RVators had a sketch and infor on this, I'm sure Van can send you something. Wayne RV-4 fairings. Joe Wiza wrote: > > Friend of mine bilding an RV4 can't find any info on PN F-482 left and > right. Does anyone know where they go or better print #. TU > > planejoe(at)ewol.com > ________________________________________________________________________________
Date: Jan 21, 2000
From: Andrew Bond <ahb(at)cisco.com>
Subject: Flying an RV-8 with the "top down"
I know the RV-8 is not designed to be flown with the canopy opened, but what if it were removed completely, like an open cockpit. Could it be flown in this configuration? If so how safe would it be? Has anyone tried it? Any ideas/feedback appreciated. Andrew Bond ahb(at)cisco.com RV-8, Planning Stage ________________________________________________________________________________
Date: Jan 21, 2000
From: Gary Zilik <zilik(at)bewellnet.com>
Subject: Re: Firewall questions
Doug Instead of using the standard Concord battery you might try using the Odyssey battery listed in Van's catalogue. Not only is it lighter, it's also half the size with the approx. the same capacity. The warranty is also longer than the average life of a concord. This would allow a smaller battery box on the firewall. Gary Zilik RV-6A N99PZ ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Flying an RV-8 with the "top down"
Date: Jan 21, 2000
>I know the RV-8 is not designed to be flown with the canopy opened, but >what if it were removed completely, like an open >cockpit. Could it be flown in this configuration? If so how safe would it >be? Has anyone tried it? Any ideas/feedback >appreciated. > >Andrew Bond >ahb(at)cisco.com >RV-8, Planning Stage Andrew, Sorry, interesting concept, but I can't see that as being feasible or safe. These are FAST airplanes, and not meant for lazy cruising around the patch on a summer day at 80mph. Rest assured though, when the cooling air vent is opened up, it puts out a LOT of air! I opened it up fully for the first time two days ago, and it about blew the chart off my lap. :) Brian Denk RV8 N94BD 21.5 hours. ________________________________________________________________________________
From: HillJW(at)aol.com
Date: Jan 21, 2000
Subject: canopy seal
I have a lot of air coming in arount the canopy skirt on my 8a. If I put enough weather strip in to help, it sticks the canopy down so that it is hard to open---won't slide back enough to raise up. Anyone figured out a good remedy? hilljw(at)aol.com rv8a ________________________________________________________________________________
From: Elrod3794(at)aol.com
Date: Jan 21, 2000
Subject: elevator stop
After mounting the horizontal stab. And installing the elevators and the push/pull tube. I have 25degeree up travel and 28degree down and not any room for the elevator stop. the elevator horn, stops against the (F812C)angle. I can not see where it would be a problem. does anyone know why i have to install the elevator stop vans planes call for thanks for any help Mike erode 8a-qb any builders from Birmingham area on the list ________________________________________________________________________________
From: "Rob Reece" <reece(at)rt66.com>
Subject: Flying an RV-8 with the "top down"
Date: Jan 21, 2000
There was an open cockpit RV-3 built by a man named John Williams, of Waco, TX (could scan a picture of two if you'd like). It was N112KW, and first flew in 1980. The canopy was replaced with a Pitts style windshield. These are the spec that were given: Engine: O-320-H2AD 160 hp Prop: Sensenich metal 70x70 Empty weight: 724# w/ full electric Top speed: 195mph at 2875 rpm (3500'msl) It was mentioned that cruising above 150mph was "uncomfortable." I can only imagine. I did talk to Jess Mallian at Copperstate this last fall , a RV-3 owner who recently lost his -3 canopy in-flight. It was in John Harmon's 3rd built RV-3, 33RV that he had purchased. Jess said it flew fine, but was really loud and turbulent. Jess was fortunate. . the canopy lifted off and nicked him in the forehead and then continued rearward and struck the vertical stab chipping the paint off of the fiberglass tip. i would think if you could beef up the canopy/latch on the -8, that it could be flown in this configuration without any major controllability problems. . . just drag and noise issues. Rob Reece RV-3 SN45 re-skinning wings > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Andrew Bond > Sent: Friday, January 21, 2000 5:26 PM > To: rv-list(at)matronics.com > Subject: RV-List: Flying an RV-8 with the "top down" > > > I know the RV-8 is not designed to be flown with the canopy > opened, but what if it were removed completely, like an open > cockpit. Could it be flown in this configuration? If so how safe > would it be? Has anyone tried it? Any ideas/feedback > appreciated. > > Andrew Bond > ahb(at)cisco.com > RV-8, Planning Stage > > ________________________________________________________________________________
From: "Rick Caldwell" <racaldwell(at)hotmail.com>
Subject: Re: elevator stop
Date: Jan 21, 2000
Mike, I had to trim some off the steel elevator horn in order to get the travel for my -6. I think this is normal. I filed the horn so it hit the stops I put in flush across its width (height). Rick Caldwell RV-6 N136RC 1.3 hrs Melbourne, FL >From: Elrod3794(at)aol.com >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: elevator stop >Date: Fri, 21 Jan 2000 21:02:50 EST > > >After mounting the horizontal stab. And installing the elevators and the >push/pull tube. >I have 25degeree up travel and 28degree down and not any room for >the elevator stop. > the elevator horn, stops against the (F812C)angle. >I can not see where it would be a problem. >does anyone know why i have to install the elevator stop vans planes call >for >thanks for any help >Mike erode 8a-qb >any builders from Birmingham area on the list > > ________________________________________________________________________________
From: MarkVN(at)aol.com
Date: Jan 21, 2000
Subject: Re: Flying an RV-8 with the "top down"
unsubscribe ________________________________________________________________________________
From: "jfarrar1" <jfarrar1(at)home.com>
Subject: Re: Electroair ignition
Date: Jan 21, 2000
Great Bob, thanks a bunch, this is what I was looking for. So I could wire it to the battery side of my essential bus switch...the one that connects the e-bus to the battery direct??? Jeff calls for shielded conductor for noise, do you see this as necessary? Jeff Farrar, RV8A N4ZF reserved, Chandler, AZ jfarrar1(at)home.com Wings done, fuselage almost, fuselage interior and wiring. > > The running load for Jeff's ignition system is under 1 amp. > He shows 18AWG wire to hook it up for voltage drop considerations . . . > which are obviously very tiny. The system does have an inrush > current on the order of 7-8 amps when you first turn it on. > > Given that it's an electronic ignition, it should be wired to > the always hot side of the battery contactor . . . it needs to > run even if the DC power master switch is OFF. Use a 22AWG > fusible link to drive 18AWG feedwire to the ignition toggle > switch. > > > Bob . . . > ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 21, 2000
Subject: Re: Scott McDaniels
In a message dated 1/21/00 8:07:13 AM Pacific Standard Time, cdaniel(at)fnbbaldwin.com writes: << Several times I have had conversations with the folks at Vans and gotten advice that contradicted what I had heard from the listers. When I brought this to the attention of the Vans folks, I got the distinct impression that a lot of misinformation flows from the listers. >> Frankly I might have agreed, but some of the information Van's has given thru the RVator in the past didn't square with reality either. There are gaps in the info and disinformation from both groups. That is why it's not an "us or them" choice. You need to keep your ear to the ground. -GV ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 21, 2000
Subject: Re: Scott McDaniels
In a message dated 1/21/00 2:56:34 PM Pacific Standard Time, SportAV8R(at)aol.com writes: << I cannot think of anything more valuable to the list membership, and indirectly, to Van's Aircraft, Inc., than an official (or nearly so) voice from the factory on this list. >> I also would like there to be someone(s) on the list to speak in an official capacity for Van's. Scott was a great contributor even though I didn't always concur with his posts (everyone sees a different reality). The problem is that the factory has certain opinions that they often advance which are not terribly helpful. "Just make it work" comes to mind. People on the list can tell you HOW to make it work. -GV. ________________________________________________________________________________
From: "Ted French" <ted_french(at)canada.com>
Subject: Re: Accesories & Instrument Panel
Date: Jan 21, 2000
Drill & tap the holes into the panel Ted French Prince george BC RV-6A flying ----- Original Message ----- From: George McNutt <gmcnutt(at)intergate.bc.ca> Sent: Thursday, January 20, 2000 11:18 PM Subject: RV-List: Accesories & Instrument Panel > > Trying to design for future maintainability, getting lazy in my old age. > > I am presently in the process of cutting and drilling holes in my > instrument panel and have discovered some of the components are supplied > with tiny attachment nuts and screws making future removal/replacement > for repairs very difficult. > > For example, the electric trim switch and LED indicator units are > supplied with number two screws and nuts, the ELT monitor is designed > for #4 screws & nuts. > > As these components are not designed into the removable portion of my > panel, and some clearances are tight, I can imagine myself trying to > crawl under the panel in a few years and trying to start a #2 nut in the > semi darkness. Heck I can hardly see the thing on the workbench today. > > Checking Aircraft Spruce & Wicks catalogs I find no plate-nuts or > similar attachments smaller than #6 so I am thinking of making > individual collars to fit behind the inst. panel and around the > components, rivited on and with threaded holes for the screws. > > However before I go to all that trouble I thought I would ask for the > wisdom of RV-Listers for any simpler solutions or ideas. > > George McNutt > 6-A inst pnl > Langley, B.C. > > > > > ________________________________________________________________________________
From: BrooksRV6(at)webtv.net (Chris Brooks)
Date: Jan 21, 2000
Subject: Engine Baffles
I started installing my baffle kit from Vans and the cut-outs in the side pieces don't clear the rocker covers, also the holes for the 2 screws that secure them to the cylinders don't line up. They're about 1/2 a hole off and not all in the same direction. I'll have a figure 8 hole in each piece if I use them. Are these pieces typically this bad, or did I get a bad kit? Chris Brooks RV6 ________________________________________________________________________________
From: "Dennis Persyk" <dpersyk(at)worldnet.att.net>
Subject: Re: Engine Baffles
Date: Jan 21, 2000
Unfortunately the misfit is typical. However you will put doublers over many of the holes so the holes in the doublers can be correct. The pieces seem to be laser cut and are probably mis-cut to the nearest 0.0001 inch! (And if you call Van's they will swear you are the first one to ever have this problem.) Dennis Persyk 6A finishing kit Hampshire, IL C28 -----Original Message----- From: Chris Brooks <BrooksRV6(at)webtv.net> Date: Friday, January 21, 2000 10:44 PM Subject: RV-List: Engine Baffles > >I started installing my baffle kit from Vans and the cut-outs in the >side pieces don't clear the rocker covers, also the holes for the 2 >screws that secure them to the cylinders don't line up. They're about >1/2 a hole off and not all in the same direction. I'll have a figure 8 >hole in each piece if I use them. Are these pieces typically this bad, >or did I get a bad kit? > Chris Brooks RV6 > > ________________________________________________________________________________
Date: Jan 21, 2000
From: Doug Shenk <dshenk(at)ruralhealth.org>
Subject: Re: Scott McDaniels
Would anyone besides me like to see a moderated RV-list for builders who want to just exchange information about building? Perhaps a separate list could be established for those posts that relate more to the politics and opinion wars that seem to have dominated much of the list lately. I'm sorry to see a lot of good posters leave the list out of frustration and being attacked. Do not archive. Doug Shenk, RV6A-QB ________________________________________________________________________________
Date: Jan 21, 2000
From: "dgmurray" <dgmurray(at)telusplanet.net>
Subject: Re: Engine Baffles
Subject: Re: RV-List: Engine Baffles > >Unfortunately the misfit is typical. However you will put doublers over >many of the holes so the holes in the doublers can be correct. The pieces >seem to be laser cut and are probably mis-cut to the nearest 0.0001 inch! >(And if you call Van's they will swear you are the first one to ever have >this problem.) >Dennis Persyk 6A finishing kit > Dennis - I must have got lucky because all to holes lined up right on. I am using a 0-360-A4M and it might make a difference for the other models of engines. In any case I was really impressed with the quality of the kit. Doug Murray RV-6 Southern Alberta ________________________________________________________________________________
From: "Ginmarcus" <Ginmarcus(at)econophone.ch>
Subject: Re: RV's at Meadowlake Airport, 00V, in Peyton Colorado...
Date: Jan 22, 2000
Dear Bill May I ask you if there are any RV's for sale at your airport ? I am pretty new to the RV scene and looking around to buy either RV-3 or RV-4. Thanks very much for your info Marc ----- Original Message ----- From: Bill VonDane <bvondane(at)atmel.com> Sent: Friday, January 21, 2000 8:45 PM Subject: RV-List: RV's at Meadowlake Airport, 00V, in Peyton Colorado... > > Hello All... > > I don't wish to get too off topic here, but all the talk lately about places > to fly to spurred me to tell you all about our little airport... EAA > Chapter 72 - http://eaa72.tripod.com is based at Meadowlake Airport - 00V, > in Peyton, CO, just 14nm (26km) NE of Colorado Springs, at a field elevation > of 6874 ft. > > We have more than 6 flying RV's, and more than 8 under construction at this > time... I have added a page to my web site with information about the RV's > and RV builders at our airport, and encourage you to take a look... > http://vondane.tripod.com/colorv/ > > We try to have a little cook-out / get together on the Saturday after the > 3rd Tuesday of each month, which just happens to be tomorrow for January. > We'll be there from 9:00am till 1:00pm, and probably longer... > > If you in the neighborhood, drop in, say hey, and have a burger! I > understand we're gonna have a few Russian aircraft visiting us tomorrow... > On your way in, just let us know your inbound for an EAA burger, and we'll > help you get to the right hanger... > > Thanks... > > -Bill Von Dane - Colorado Springs, CO > RV-8A N912V res., waiting for wings > http://vondane.tripod.com > > ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Jan 22, 2000
Subject: Re: Scott McDaniels
In a message dated 1/21/2000 11:30:10 PM Central Standard Time, dshenk(at)ruralhealth.org writes: << Would anyone besides me like to see a moderated RV-list for builders who want to just exchange information about building? Perhaps a separate list could be established for those posts that relate more to the politics and opinion wars that seem to have dominated much of the list lately. I'm sorry to see a lot of good posters leave the list out of frustration and being attacked. Do not archive. Doug Shenk, RV6A-QB >> I do have one question on this. What about Rocket builders, would i become persona non grata on this list. Also how would moderate it. Chris Wilcox F-1 Rocket ________________________________________________________________________________
Date: Jan 22, 2000
From: EARL FORTNER <e.fortner(at)worldnet.att.net>
Subject: Re: RV4, F-482
That is the rear seat reinforcement. Call Vans and tell them you want the service bulletin and kit for the rear seat reinforcement. They will send you everything you need at no charge. Joe Wiza wrote: > > > Friend of mine bilding an RV4 can't find any info on PN F-482 left and > right. Does anyone know where they go or better print #. TU > > planejoe(at)ewol.com > ________________________________________________________________________________
From: "Joe Wiza" <planejoe(at)ewol.com>
Subject: Cross Country
Date: Jan 22, 2000
N63980, RV6A, O360, CSP just finished its 2ND X country Venice FL to PHX AZ and back (Over 4,000 miles) total time on ACFT now 66 hrs. Other then adding two quarts of oil, fuel and cleaning the windshield no problems encountered. I personnally have to experience something to believe and in my opinion I beleive now that this is a great X country ACFT. The view out of the bubble canopy was spectacular especially crossing New Mexico and Arizona. We used radar flight following most of the way (These folks earn their money). We got several nice complements from the controllers about the speed ETC. A couple of the guys ABQ center said they were building RV'S. We encountered cross winds once that were a little to breezy for my taste but keeping the wing down into the wind and the longitudinal axis parallel with the runway ,everything worked out fine. Well anyway keep on buckin it's worth it. do not archieve planejoe(at)ewol.com ________________________________________________________________________________
From: "Jerry Carter" <rv8abuild(at)mindspring.com>
Subject: 8A Step, Flap fairing
Date: Jan 22, 2000
For those of you building the 8A QB and installing the step, I will share this. I installed the step earlier in construction. I realize this is a mistake now because of the step's penetration of the F-872C-L flap fairing. As I understand it, the sequence of installation should be: 1)Install wing root fairings 872A & B. 2)Mark flap fairing so that it is flush against the top of the fully retracted flap. 2)Take the flap bar and floors out and drill the forward part of the 872C L & R from the inside of the fuselage thru pre-drilled holes in the fuselage. 3)Line up the aft part of the 872C-R so that the forward edge of the aft part is paralell to the flap as in view E-E in drawing 43, and drill thru the pre-punched holes in the right fairing only.4)Install the step. 5)Make a template of the F-872-L out of cardboard or 020 so that you can figure out where to drill the hole where the step goes thru the fairing. 6)Cut the hole for the step in the left fairing, install it, then drill the holes in the aft part as you did for the right one in step 3 above. Note where the step penetrates the fairing. It is ABOVE the crease in the fairing. I took videos of the factory 8A, and I noticed that the step goes thru the bottom of the fairing. I also noted that the fairing completely covers the step weldment. This is not the case in our kits. I called Vans yesterday about this and spoke with Ken Kruger (sp?), who designed the step. He confirmed for me that the fairing is different on the prototype 8A and that the fairing will, in fact, go across the WD 832 weldment just as depicted in drawing 24A in the "Isometric View" on the left of the page. I found it interesting that the rivets called for on the weldment are all AN470AD4's instead of flush rivets. When I installed the step, I did not think anything about it since I expected all the rivets to be covered by the fairing. Ken said that it would be OK to replace these rivets with flush rivets. So, I would recommend using 426 rivets on the top two rows of rivets on the weldment, although I guess it's only a matter of cosmetics. If you already installed the step, like I did, then you have to figure out how to get the left flap fairing lined up on top of the flap before you cut the hole for the step. I'm gonna make an aluminum trial fairing today and see if I can make it work. Any other helpful suggestions would be appreciated. Jerry Carter 8AQB ________________________________________________________________________________
From: "Bill & Debi VonDane" <vondanes(at)hotmail.com>
Subject: Re: RV's at Meadowlake Airport, 00V, in Peyton Colorado...
Date: Jan 22, 2000
Right now there is only 1/2 interest in an RV-4 for sale... 1/2 ownership in 1995 RV-4 100TT and SMOH, 150HP, FP, Full panel, Leather Interior, Meadowlake, $25K Contact Dave Hirschman, 719-636-0274 Bill Von Dane, Colorado Springs, CO RV-8A N912V (res), waiting for wing kit http://vondane.tripod.com Dear Bill May I ask you if there are any RV's for sale at your airport ? ________________________________________________________________________________
From: WFACT01(at)aol.com
Date: Jan 22, 2000
Subject: Re: Scott McDaniels
Gee, really sorry to see Scott and Mark leave the list...Many of us OSHKOSH and SUN-n-FUN winners read the list--but will not give their opinions on what they are building and what mods and changes they are making because of unfounded, unsubstantiated criticisms. The only ones who lose out are the good people on the list who are seeking sound advice and new ideas. Tom RV-8, IO540 Lycoming ________________________________________________________________________________
Date: Jan 22, 2000
From: Kevin Horton <khorton(at)cyberus.ca>
Subject: Moderated list, was Scott McDaniels
> >Would anyone besides me like to see a moderated RV-list for builders >who want to >just exchange information about building? I also get frustrated at all the posts about stuff other than building (posts complaining about whiners have no more do about building than the whiner's posts, if you think about it - not a flame, just an observation). But, a moderated list is not really the answer. A moderated list requires a moderator to look at each post and send it to the list, rejecting the trash. But, who wants to be the moderator? And the list stops whenever the moderator sleeps, eats or goes to the bathroom. I will take the current list, with the quick response to questions, over a moderated list any day. You don't have to ready everything that is on the list. I'm pretty quick to hit the delete key if the subject doesn't interest me, or if the poster has never had anything useful to say before. Sure, I probably miss a few gems that way, but I save myself lots of frustration. Please send any flames direct to me. Take care, Kevin Horton RV-8 (fuselage in the jig) Ottawa, Canada http://members.xoom.com/kevinhorton/rv8.html ________________________________________________________________________________
From: "John B. Holmgreen" <j32619(at)innova.net>
Subject: Re: Engine Baffles
Date: Jan 22, 2000
----- Original Message ----- From: dgmurray <dgmurray(at)telusplanet.net> Sent: Saturday, January 22, 2000 12:50 AM Subject: Re: RV-List: Engine Baffles > > > Subject: Re: RV-List: Engine Baffles > > > > > >Unfortunately the misfit is typical. However you will put doublers over > >many of the holes so the holes in the doublers can be correct. The pieces > >seem to be laser cut and are probably mis-cut to the nearest 0.0001 inch! > >(And if you call Van's they will swear you are the first one to ever have > >this problem.) > >Dennis Persyk 6A finishing kit > > > > Dennis - > I must have got lucky because all to holes lined up right on. I am > using a 0-360-A4M and it might make a difference for the other models of > engines. In any case I was really impressed with the quality of the kit. > > Doug Murray RV-6 > Southern Alberta > Dennis, I have an O-360-A4N , and mine fit perfectly too. Maybe there is enough variation in engine types to affect the kit? John Holmgreen Clinton SC RV-6A flying > > ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: 540
Date: Jan 22, 2000
> Tom RV-8, IO540 Lycoming Any new news on your flight testing? Larry Bowen RV-8 tanks Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: canopy seal
Date: Jan 22, 2000
>From: HillJW(at)aol.com >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: canopy seal >Date: Fri, 21 Jan 2000 20:51:27 EST > > >I have a lot of air coming in arount the canopy skirt on my 8a. If I put >enough weather strip in to help, it sticks the canopy down so that it is >hard >to open---won't slide back enough to raise up. > >Anyone figured out a good remedy? > >hilljw(at)aol.com >rv8a I'm using adhesive backed felt that I found in 8x11" sheets at a craft store. It doesn't drag the canopy down and is very gentle on the surface of the turtledeck. It's been holding up pretty well but the summer heat will be the real test of the adhesive. Brian Denk RV8 N94BD 21.5 hours. Prop get's balanced today. ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: elevator stop
Date: Jan 22, 2000
> > >After mounting the horizontal stab. And installing the elevators and the >push/pull tube. >I have 25degeree up travel and 28degree down and not any room for >the elevator stop. > the elevator horn, stops against the (F812C)angle. >I can not see where it would be a problem. >does anyone know why i have to install the elevator stop vans planes call >for >thanks for any help >Mike erode 8a-qb >any builders from Birmingham area on the list Mike, My -8 is the same way. I did not put in an elevator stop. It passed inspection and is flying great. Brian Denk RV8 N94BD ________________________________________________________________________________
From: "John B. Holmgreen" <j32619(at)innova.net>
Subject: RMI Monitor Fuel Sensor
Date: Jan 22, 2000
For those of you using the RMI fuel flow sensor......I experience an increase of approximately 2 GPH fuel flow at cruise settings when I turn on the electric fuel boost pump and it returns to what I compute as "normal" fuel flow when I turn the boost pump off. Fuel pressure reads 6PSI (@6500 msl) with the engine driven pump and 7 with the electric boost pump on. The sensor is mounted on the sidewall, just rear of the rudder pedals. (RV-6A) The boost pump is mounted on the wing spar and I have about 20" of tube with a very gradual 90 degree bend with about 6" of straight tube length prior to the sensor. Any experience out there with a possible solution? If not, guess I'll have to call Ron on Monday. He's always been very patient and helpful in the past. Thanks, John Holmgreen Clinton, SC -6A with 10 hrs. and climbing. ________________________________________________________________________________
Date: Jan 22, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: Engine Baffles
The baffle kit and instructions are manufactured by a vendor for Van's. I have a NARROW deck O-320 B2B using SUPERIOR cylinders with low s/n's. I had one of the first baffle kits that sold. I experienced fitting problems and did phone and WRITE Van's with my observations and recommendations. That is how I found out that a vendor did everything with the baffles. Over the past 5 years since I purchased / fit my baffles, there have been 5 other RV builders at my airport that have purchased the baffle kit and theirs fit MUCH better than what mine did. The fustration that I experienced fitting my baffles had me say that I would build them from scratch next time. Having seen how they fit now, I would purchase the kit and make it fit. The only recommendation that I have regarding fitting baffles to the engine, is to make a cardboard template where the baffle goes against the engine and then use the template as a guide to cut the baffle. IMHO, this will save time in the long run. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
Date: Jan 22, 2000
From: Doug Shenk <dshenk(at)ruralhealth.org>
Subject: Re: Moderated list, was Scott McDaniels
Sorry I brought this up. I'm guilty of "whining" about the "whining." I have my delete so will just be quiet and get back to building and reading the building posts. Just needed to vent my frustration about the loss of major listers since I've started. I'm just looking forward to someday finishing and flying a great airplane. Doug Shenk, RV-6A, QB Kevin Horton wrote: > > > > > >Would anyone besides me like to see a moderated RV-list for builders > >who want to > >just exchange information about building? > > I also get frustrated at all the posts about stuff other than > building (posts complaining about whiners have no more do about > building than the whiner's posts, if you think about it - not a > flame, just an observation). > > But, a moderated list is not really the answer. A moderated list > requires a moderator to look at each post and send it to the list, > rejecting the trash. But, who wants to be the moderator? And the > list stops whenever the moderator sleeps, eats or goes to the > bathroom. I will take the current list, with the quick response to > questions, over a moderated list any day. > > You don't have to ready everything that is on the list. I'm pretty > quick to hit the delete key if the subject doesn't interest me, or if > the poster has never had anything useful to say before. Sure, I > probably miss a few gems that way, but I save myself lots of > frustration. > > Please send any flames direct to me. > > Take care, > Kevin Horton RV-8 (fuselage in the jig) > Ottawa, Canada > http://members.xoom.com/kevinhorton/rv8.html > ________________________________________________________________________________
Date: Jan 22, 2000
From: Kevin Horton <khorton(at)cyberus.ca>
Subject: Re: RMI Monitor Fuel Sensor
> > For those of you using the RMI fuel flow sensor......I experience an >increase of approximately 2 GPH fuel flow at cruise settings when I turn on >the electric fuel boost pump and it returns to what I compute as "normal" >fuel flow when I turn the boost pump off. > > Fuel pressure reads 6PSI (@6500 msl) with the engine driven pump and 7 >with the electric boost pump on. > > The sensor is mounted on the sidewall, just rear of the rudder pedals. >(RV-6A) The boost pump is mounted on the wing spar and I have about 20" of >tube with a very gradual 90 degree bend with about 6" of straight tube >length prior to the sensor. > > Any experience out there with a possible solution? If not, guess I'll have >to call Ron on Monday. He's always been very patient and helpful in the >past. > John, For what it's worth, I recall others have reported the same effect. The best theory seemed to be the turbulence and/or pressure pulsations from the boost pump were changing the calibration of the sensor. These things need the "k" factor adjusted to make them read accurately in each installation, and it just may be that you would need a different "k" factor with the boost pump ON, than if the boost pump is OFF. Of course, you can only have one "k" factor, so it will read wrong in one of these situations. Wouldn't it be nice if someone would make a fuel computer with provisions for two "k" factors, with an input from the boost pump switch to tell it which "k" factor to use. Sounds like a marketing opportunity for someone. Matt? Take care, Kevin Horton RV-8 (landing gear boxes) Ottawa, Canada http://members.xoom.com/kevinhorton/rv8.html ________________________________________________________________________________
From: "marcel de ruiter" <marcelderuiter(at)email.msn.com>
Subject: Re: Engine Baffles
Date: Jan 22, 2000
> > Subject: Re: RV-List: Engine Baffles > > >Unfortunately the misfit is typical. I don't know a lot about the baffles that VAN'S sell, but I do know that lyc320 & lyc360 vary in shape and size. I believe this caused by the different letter and number combinations after the engine size. Is it maybe that VAN'S only make baffles for the particular lycomings they sell?I.E. lyc IO 360-A1B6, lyc O 320-D1A, lyc 360-A1A. It seems to me that you have a different engine than the ones that VAN'S sell. What is VAN'S response to this? Marcel de Ruiter RV4/G-RVMJ ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Jan 22, 2000
Subject: Re: Palm Pilot
In a message dated 1/22/2000 10:55:02 AM Central Standard Time, GLPalinkas(at)aol.com writes: << www.palm.com - info on models www.outpost.com - best price Sorry forgot to add: www.infoequipt.com - best E6B simulator (Aircalc lite & pro....works great, no affiliation) In a message dated 1/22/00 11:32:34 AM, tripod(at)oneimage.com writes: << Hi Listers, Does anyone have a web page for the manafacturer of the Palm Pilots? Also a web site for purchase of same. Bruce Knoll >> Also look at www.handspring.com This company is owned by the 2 people who designed the palm for 3com. It is 100% compatable with the palm. It is also cheaper, alot cheaper. In fact I was going to buy a handspring tell and insurance company that i work with gave us palm V's. So know I have a Palm V. But I would look at handspring if you want to save some money Chris Wilcox F-1 Rocket ________________________________________________________________________________
From: N188sm(at)cs.com
Date: Jan 22, 2000
Subject: Re: Scott McDaniels
Perhaps someone could act as police and restrict anyone who does not stick to builder subjects. Stan Mehrhoff RV-8 to fly next week, another one mounting engine on. ________________________________________________________________________________
From: Metalplane(at)aol.com
Date: Jan 22, 2000
Subject: RV COMM Freq vote
I like the idea of picking a manufacturer's test frequency as the "RV Channel": 123.125 - 123.275 or 123.325 - 123.475 or 123.525 - 123.575 We are the manufactures and I don't think Cessna would mind. Somebody pick one!!!!!!!!!!! ________________________________________________________________________________
From: WFACT01(at)aol.com
Date: Jan 22, 2000
Subject: Re: 540
LARRY JUST GOT MY CARBON FIBER COWLS TRYING TO MAKE SUN AN FUN TOM IO540 ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Palm Pilot
Date: Jan 22, 2000
Try http://Onvia.com if you want to buy one on-line. I've bought several things from them, including my Kodak DC240 digital camera. Fair prices and free shipping too. Larry Bowen RV-8 tanks Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > > Hi Listers, > > Does anyone have a web page for the manafacturer of the Palm Pilots? Also > a web site for purchase of same. > > Bruce Knoll ________________________________________________________________________________
From: wvu(at)mail.ameritel.net
Date: Jan 22, 2000
Subject: Re: Scott McDaniels
Perhaps I could offer some motherhood on this subject. I didn't even built my -6 and am enjoying the opinions of this group intensely. I mean just that, opinions. In the year or so following the discussions in this group I have seen happy attitudes, sad attitudes, frustrations, and a few toes were accidentally stepped on. But nevertheless all opinions were genuine. I think everyone is entitled to an opinion. Everyone is also entitled to choosing what he wants to listen/ respond to (and either enjoy or suffer the concequences accordingly). I was not born in the States and I have come to love this country for what it can "see" that many countries can't - freedom of speech. Yes I can recite many bad things which are direct results of this very belief. But I think the goods outweighs the bads. I'm willing to keep this belief - the choice to express oneself. It's a good thing. I still enjoy this list. Anh N985VU Marylnd > >Perhaps someone could act as police and restrict anyone who does not stick to >builder subjects. > >Stan Mehrhoff >RV-8 to fly next week, another one mounting engine on. > > ________________________________________________________________________________
Date: Jan 22, 2000
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Re: Scott McDaniels
> >Perhaps someone could act as police and restrict anyone who does not stick to >builder subjects. Oh, ho, ho!!! Ah, ha, ha. You ought to put in a smiley tho, Stan, some might think you serious and have you removed!! :-) hal ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Prop Balancing
Date: Jan 22, 2000
Listers, Brian Denk and I both took our RVs to New Mexico Aircraft Propeller in Belen NM today to get them dynamically balanced. I found it very interesting although David, the owner said "it isn't rocket science." For those of you that haven't seen this I will give a brief summary: Take top cowl off engine and attach vibration sensor to engine with cables running out to the display unit. Run engine at full power (in our case, and in our case with Sensenich 72FM8 props and O-360s it was 2130 RPM at 5300 MSL and about 60 degrees) while vibration is read. The vibration is given in ips, which I believe he said is impulses per second. No amplitude is measured. If the vibration is below .2 ips nothing is done, if it is higher washers are screwed temporarily to the spinner using spinner mounting screws. These weights are put at an arbitrary location as there is no phase detection either. If the vibration is worse on the next run the weights are moved 180 degrees, if it is better the weights are fine tuned by trial and error. When a final location is determined a bit more weight is added and then all the weights are moved inboard to the spinner bulkhead where they are secured with a bolt and nut through a newly drilled hole. The bit more weight is because of the move inboard. Whenever I have posted about the breaking of cowl mount hinges and exhaust supports people have e-mailed me about getting the prop balanced. I think that is a good response, but I have always felt it was quite smooth. I have also gotten e-mail indicating 72FM8 props are delivered out of balance. Well, to put it to rest I had to have it balanced. The facts in this case. Brian Denk's vibration was at .1 ips or below. As smooth as it comes according to the prop guy. Smoother than a lot of turboprops. The lucky SOB! He still notes his fire extinguisher trembling a bit though. My vibration was about .4 ips. Quite smooth but at a level where it can be improved. He got mine to between .1 and .2 ips. I think I can tell a difference in flight, but probably could not swear to it on a stack of Bibles. Any further breakage, at least I will know it is not vibration. Larry Pardue Carlsbad, NM RV-6 N441LP http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
From: "Jerry Carter" <rv8abuild(at)mindspring.com>
Subject: Re: Palm Pilot
Date: Jan 22, 2000
Try www.igo.com Jerry Carter > > ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: RMI Monitor Fuel Sensor
Date: Jan 22, 2000
> John, > > For what it's worth, I recall others have reported the same effect. > The best theory seemed to be the turbulence and/or pressure > pulsations from the boost pump were changing the calibration of the > sensor. >Take care, >Kevin Horton Could the sensor be enough of a restriction such that it is cavitating a little when fuel is pulled through it in a pulsatile manner, as the engine driven pump does? The pressure in the sensor would be something less than atmospheric when only the engine pump is on. However, in the case where the boost pump is before the sensor and on, the sensor pressure would be full system pressure. Perhaps this is what is going on. I guess the ideal place for the sensor would be between the engine pump and carb/injection, but this would require an additional hose. Alex Peterson Maple Grove, MN 6A ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Re: Prop Balancing
Date: Jan 22, 2000
> > Any further breakage, at least I will know it is not vibration. > > Larry Pardue > Carlsbad, NM > > RV-6 N441LP Further breakage is likely to be caused by vibration, but not due to imbalances in the engine. The whole cowl can be thought of as a large collection of springs, each with its own natural frequency. If one could magically "see" inside the cowl when in flight, it might be surprising (or scary). I don't know specifically where your cowl hinges are breaking, but is it possible to fashion small brackets with rubber feet, which, when mounted to the firewall, apply some pressure outward on the cowl right near the hinge? Somehow, the natural frequency of the cowl in the area of breaking hinges needs to be changed, as it might be the same frequency as the prop pulses. Maybe glassing stiffener ribs in the cowl in the region of interest would also help. Just thoughts on what might help, not claiming they will work! Alex Peterson ________________________________________________________________________________
From: "Karl Ahamer" <ascot(at)hinet.net.au>
Subject: Re: RMI Monitor Fuel Sensor
Date: Jan 23, 2000
I also get a higher reading of fuelflow with the electric pump on .I think this problem was discussed on the list some time ago.The higher reading is apparently caused by the pressure pulses generated by the boost pump... RV6AQ VH-KHA 31 Hours KARL AHAMER NSW AUSTRALIA ASCOT(at)HINET.NET.AU ________________________________________________________________________________
From: "Bryan E. Files" <bfiles(at)corecom.net>
Subject: Prop Balancing
Date: Jan 22, 2000
FWIW, I have noticed that on all the aircraft that I have had the propellers balanced on it took away the low frequency vibrations and there were more noticeable high frequency vibrations. Though it did feel better flying the aircraft. I am not sure on your cowl but usually high freq. vibrations cause cracking. ***Bryan E. Files*** A&P, IA, FAA Safety Counselor Fat City Aircraft Palmer, Alaska mailto:BFiles(at)corecom.net ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 22, 2000
First. ips is inches per second which refers to accelerometers which measure acceleration in distance.( there also are velometers which work off of velocity). The "ips" reading IS your amplitude, or more simply the strength of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable vibration) you have a lazy mechanic. If washers are placed arbitrarily you again are dealing with a idiot. The system is simple. The accelerometer can only measure vibration in one plane, so it is pointed to the center of crank in plane with prop and as close as possible to it. The accelerometer not only gives a strength reading but also a "phase angle" reading which sends the appropriate signal to the strobex flasher. Reflective tape is placed on prop ( I put a piece on each blade of different shape in case subject blade is where I could not see). When pointing the strobe at prop while running you note where tape is. Aircraft is shut down and the prop put back where you saw it. Here is the simple fact. The accelerometer ALWAYS wants the wieght put accross from it since the accelerometer is signaling a flash when heavy part is NEXT to it. So you put some weight accross from where the accelerometer is (when blade is as observed with flash) and aircraft run again. If you were .4 and now are .2 and blade is in same place as before, you only added 1/2 of amount necessary. I do not stop until I get the lowest reading. The newer equipment also mounts a accelerometer back on the accessory case. Reason is if vibration here gets better as prop gets better you are ok. If case gets worse as prop gets better, you have problems other than prop. Bent crank or other items. I want to make it clear I do not want to flame you, but vibration and the methods to control it are serious and I want people to understand this. Oh yeah, I know this from 20 years of doing this on helicopters ( lots of rotating stuff!). Bill N. RV4 flying. PPSEL.A&P-IA, Chief Inspector and many other things not as intresting. -----Original Message----- From: Larry Pardue <n5lp(at)carlsbad.net> Date: Saturday, January 22, 2000 6:13 PM Subject: RV-List: Prop Balancing > >Listers, > >Brian Denk and I both took our RVs to New Mexico Aircraft Propeller in Belen >NM today to get them dynamically balanced. I found it very interesting >although David, the owner said "it isn't rocket science." > >For those of you that haven't seen this I will give a brief summary: Take >top cowl off engine and attach vibration sensor to engine with cables >running out to the display unit. Run engine at full power (in our case, and >in our case with Sensenich 72FM8 props and O-360s it was 2130 RPM at 5300 >MSL and about 60 degrees) while vibration is read. The vibration is given >in ips, which I believe he said is impulses per second. No amplitude is >measured. If the vibration is below .2 ips nothing is done, if it is higher >washers are screwed temporarily to the spinner using spinner mounting >screws. These weights are put at an arbitrary location as there is no phase >detection either. If the vibration is worse on the next run the weights are >moved 180 degrees, if it is better the weights are fine tuned by trial and >error. When a final location is determined a bit more weight is added and >then all the weights are moved inboard to the spinner bulkhead where they >are secured with a bolt and nut through a newly drilled hole. The bit more >weight is because of the move inboard. > >Whenever I have posted about the breaking of cowl mount hinges and exhaust >supports people have e-mailed me about getting the prop balanced. I think >that is a good response, but I have always felt it was quite smooth. I have >also gotten e-mail indicating 72FM8 props are delivered out of balance. >Well, to put it to rest I had to have it balanced. > >The facts in this case. Brian Denk's vibration was at .1 ips or below. As >smooth as it comes according to the prop guy. Smoother than a lot of >turboprops. The lucky SOB! He still notes his fire extinguisher trembling >a bit though. > >My vibration was about .4 ips. Quite smooth but at a level where it can be >improved. He got mine to between .1 and .2 ips. I think I can tell a >difference in flight, but probably could not swear to it on a stack of >Bibles. > >Any further breakage, at least I will know it is not vibration. > >Larry Pardue >Carlsbad, NM > >RV-6 N441LP > >http://www.carlsbadnm.com/n5lp/index.htm > > ________________________________________________________________________________
Date: Jan 22, 2000
From: David Burton <dburton(at)foxinternet.net>
Subject: Re: RV COMM Freq vote
It is my understanding that these frequencies are for manufacturers of radios, navigation equipment and the like to use during tests. Transmitting on these frequencies during a test run could ruin the test, and cost them tens of thousands of dollars. There are frequently multiple aircraft and ground stations in use during the testing... The FAA has tracked down offenders in the past and been real mean to them! The chances of that happening to most of us is vanishingly small, but it still is not a great idea to use those frequencies. Metalplane(at)aol.com wrote: > > I like the idea of picking a manufacturer's test frequency as the "RV > Channel": 123.125 - 123.275 or 123.325 - 123.475 or 123.525 - 123.575 > > We are the manufactures and I don't think Cessna would mind. > > Somebody pick one!!!!!!!!!!! > ________________________________________________________________________________
Date: Jan 22, 2000
From: Shirley Hobenshield <shobenshield(at)cmsd.bc.ca>
Subject: Skis
I am trying to get some imfo from those who may have installed skis on their RV or know of someone who did. The winter weather here has been great and I now have more time to myself where as the 6 has always been hangered till spring, time to enjoy it more! There was someone in the Yukon I believe, maybe an RV-4 that installed a set. If you are here I'd sure appreciate hearing from you. Any imfo would be great though. Thanks. Ed Hobenshield ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)carlsbad.net>
Subject: Re: Prop Balancing
Date: Jan 22, 2000
> >First. ips is inches per second which refers to accelerometers which measure >acceleration in distance.( there also are velometers which work off of >velocity). The "ips" reading IS your amplitude, or more simply the strength >of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable >vibration) you have a lazy mechanic. I certainly can not argue with you. It is apparent you know what you are talking about. I went in thinking ips stood for inches per second and specifically asked him. He said "interruptions per second" (I said I thought impulses per second in my first post, but I have since remembered), which I must admit did not make sense to me as .2 interruptions per second sounds really slow. I also asked him about amplitude and he said his system does not measure it. I expected the system to also measure phase and again he said no and that is why the first placement is arbitrary. >If washers are placed arbitrarily you >again are dealing with a idiot. The system is simple. The accelerometer can >only measure vibration in one plane, so it is pointed to the center of crank >in plane with prop and as close as possible to it. The accelerometer not >only gives a strength reading but also a "phase angle" reading which sends >the appropriate signal to the strobex flasher. Reflective tape is placed on >prop ( I put a piece on each blade of different shape in case subject blade >is where I could not see). When pointing the strobe at prop while running >you note where tape is. Aircraft is shut down and the prop put back where >you saw it. Here is the simple fact. The accelerometer ALWAYS wants the >wieght put accross from it since the accelerometer is signaling a flash when >heavy part is NEXT to it. My mechanic had a strobe system but said he does not normally use it. He said he does use it to detect dynamic tracking problems. >So you put some weight accross from where the >accelerometer is (when blade is as observed with flash) and aircraft run >again. If you were .4 and now are .2 and blade is in same place as before, >you only added 1/2 of amount necessary. I do not stop until I get the lowest >reading. The newer equipment also mounts a accelerometer back on the >accessory case. Reason is if vibration here gets better as prop gets better >you are ok. If case gets worse as prop gets better, you have problems other >than prop. Bent crank or other items. I want to make it clear I do not want >to flame you, but vibration and the methods to control it are serious and I >want people to understand this. Oh yeah, I know this from 20 years of doing >this on helicopters ( lots of rotating stuff!). Bill N. RV4 flying. >PPSEL.A&P-IA, Chief Inspector and many other things not as intresting. Thanks for all the good info. I am at kind of a loss as to what to do. I flew 500 miles up and back to the big city area to a highly recommended prop guy with a lot of experience only to find out he is an "idiot." Sometimes I feel like I can't win on this deal. I get pieces breaking and many people recommend balancing although the airplane feels smooth. I ask around and go to the professional who is recommended and get reports he is doing a bad job. Others say even if I am balanced vibrations of a different frequency will break my parts. On my professional paint job I know I got a bad job. I get my car oil changed and they put the wrong fluids in the wrong holes and break the aircleaner. There are a lot of things I am not capable of doing. If I can't go to the recommended professionals, I don't know what to do. Larry Pardue Carlsbad, NM RV-6 N441LP http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
Date: Jan 22, 2000
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Prop Balancing
Larry Pardue wrote: > > > Listers, > > Brian Denk and I both took our RVs to New Mexico Aircraft Propeller in Belen > NM today to get them dynamically balanced. I found it very interesting > although David, the owner said "it isn't rocket science." > > For those of you that haven't seen this I will give a brief summary: Take > top cowl off engine and attach vibration sensor to engine with cables > running out to the display unit. Run engine at full power (in our case, and > in our case with Sensenich 72FM8 props and O-360s it was 2130 RPM at 5300 > MSL and about 60 degrees) while vibration is read. The vibration is given > in ips, which I believe he said is impulses per second. No amplitude is > measured. If the vibration is below .2 ips nothing is done, if it is higher > washers are screwed temporarily to the spinner using spinner mounting > screws. These weights are put at an arbitrary location as there is no phase > detection either. If the vibration is worse on the next run the weights are > moved 180 degrees, if it is better the weights are fine tuned by trial and > error. When a final location is determined a bit more weight is added and > then all the weights are moved inboard to the spinner bulkhead where they > are secured with a bolt and nut through a newly drilled hole. The bit more > weight is because of the move inboard. > > Whenever I have posted about the breaking of cowl mount hinges and exhaust > supports people have e-mailed me about getting the prop balanced. I think > that is a good response, but I have always felt it was quite smooth. I have > also gotten e-mail indicating 72FM8 props are delivered out of balance. > Well, to put it to rest I had to have it balanced. > > The facts in this case. Brian Denk's vibration was at .1 ips or below. As > smooth as it comes according to the prop guy. Smoother than a lot of > turboprops. The lucky SOB! He still notes his fire extinguisher trembling > a bit though. > > My vibration was about .4 ips. Quite smooth but at a level where it can be > improved. He got mine to between .1 and .2 ips. I think I can tell a > difference in flight, but probably could not swear to it on a stack of > Bibles. > > Any further breakage, at least I will know it is not vibration. > > Larry Pardue > Carlsbad, NM > > RV-6 N441LP I am a bit perplexed by Larry's description of his prop balance technician placing weights by "trial and error"! The tech that balanced the prop on 399SB used a system that left very little to chance. If you wish to see more info and photos about this system, you can go here: http://home.HiWAAY.net/~sbuc/journal/airport5.html I found that .4 inches per second was pretty rough. The prop on my RV-6 was brought down to 0.06 ips, and it is still not as smooth as some of the other RV's in the area. However way you cut it though, dynamic prop balancing is a very good thing! Sam Buchanan "The RV Journal" http;//home/hiwaay.net/~sbuc/journal ________________________________________________________________________________
From: "Bryan E. Files" <bfiles(at)corecom.net>
Subject: Skis
Date: Jan 22, 2000
Ed, I am in the process of getting a PMA to build skis. If you want I can look into making you a set. ***Bryan E. Files*** A&P, IA, FAA Safety Counselor Fat City Aircraft Palmer, Alaska mailto:BFiles(at)corecom.net -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Shirley Hobenshield Sent: Saturday, January 22, 2000 8:05 PM Subject: RV-List: Skis I am trying to get some imfo from those who may have installed skis on their RV or know of someone who did. The winter weather here has been great and I now have more time to myself where as the 6 has always been hangered till spring, time to enjoy it more! There was someone in the Yukon I believe, maybe an RV-4 that installed a set. If you are here I'd sure appreciate hearing from you. Any imfo would be great though. Thanks. Ed Hobenshield ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 23, 2000
Subject: Re: Prop Balancing
In a message dated 1/22/00 4:39:13 PM Pacific Standard Time, n5lp(at)carlsbad.net writes: << The vibration is given in ips, which I believe he said is impulses per second. No amplitude is measured. If the vibration is below .2 ips nothing is done, if it is higher washers are screwed temporarily to the spinner using spinner mounting screws. These weights are put at an arbitrary location as there is no phase detection either. If the vibration is worse on the next run the weights are moved 180 degrees, if it is better the weights are fine tuned by trial and error. When a final location is determined a bit more weight is added and then all the weights are moved inboard to the spinner bulkhead where they are secured with a bolt and nut through a newly drilled hole. The bit more weight is because of the move inboard. >> I suggest you leave this fellow to his ignorance without looking back and find somebody that actually knows what he is doing. I had Dave Morss (of Lancair and Thunder Mustang flight testing fame) do mine and he actually has read the manuals and understands the concepts. -GV ________________________________________________________________________________
From: RobHickman(at)aol.com
Date: Jan 23, 2000
Subject: N401 Web Page Panel Photo's
I just added a Web Page with some photo's of my RV-4 and Panel http://hometown.aol.c om/robhickman/index.html Rob Hickman RV-4 N401RH (25+ Hours) ________________________________________________________________________________
Date: Jan 22, 2000
From: glenn williams <willig10(at)yahoo.com>
Subject: RV fly-in
Hey guys tommorrow on the 23rd of January there is gonna be an rv fly/get together at T67 Ft. Worth Hicks airport at Rio Concho restaurant it is to start at 1000 in the a.m. if any of you could come by I am sure that the guys would love to ogle your planes and give compliments hope to see you there Glenn Williams 8A wings FT.WORTH, TEXAS Talk to your friends online with Yahoo! Messenger.
http://im.yahoo.com ________________________________________________________________________________
From: "Paul Besing" <rv8er(at)home.com>
Subject: I sell Palm Pilots
Date: Jan 22, 2000
I work for a computer distributor. If any of you would like a Palm Pilot, I probably can get you one for what the resellers pay. Let me know off list what your costs are, and we'll see what I can get them for. I would be happy to pass these on at my cost to RV-Listers. Paul Besing RV-6A (197AB) Arizona http://members.home.net/rv8er Finish Kit ________________________________________________________________________________
Date: Jan 23, 2000
From: Denny Harjehausen <harje(at)proaxis.com>
Subject: Re: Prop Balancing
>I suggest you leave this fellow to his ignorance without looking back and >find somebody that actually knows what he is doing. I had Dave Morss (of >Lancair and Thunder Mustang flight testing fame) do mine and he actually has >read the manuals and understands the concepts. > >-GV I am looking for a prop balancer here in the Oregon area.....anyone out there know of a good one? Have a great day! Denny, RV-6 N641DH (Flying) ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: N401 Web Page Panel Photo's
Date: Jan 23, 2000
Cool engine monitor. Where did you find it? How much? Would you get it again? Larry Bowen RV-8 tanks Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of > RobHickman(at)aol.com > Sent: Sunday, January 23, 2000 1:42 AM > To: rv-list(at)matronics.com > Subject: RV-List: N401 Web Page Panel Photo's > > > I just added a Web Page with some photo's of my RV-4 and Panel > > HREF="http://hometown.aol.com/robhickman/index.html">http://hometown.aol.c > om/robhickman/index.html > > > Rob Hickman > RV-4 N401RH (25+ Hours) > > ________________________________________________________________________________
From: BrooksRV6(at)webtv.net (Chris Brooks)
Date: Jan 23, 2000
Subject: Engine Baffles responses
Some people have suggested that my baffle misfit may be because of the engine model. This is not the case, the engine is listed in the application chart for the O-360 baffle kit. Also the cut-outs, and holes in the 4 side pieces that bolt to the cylinders do not match each other. all 4 cylinders on every engine should be the same regardless of model. The response to my posting have been that others have fit from perfect to terrible. I suspect that there is some variation in the manufacturing process. I have taken a hole punch, and a file to mine and moved on. Chris Brooks RV6 ________________________________________________________________________________
From: Lothar Klingmuller <lothark(at)worldnet.att.net>
Subject: Re: Cross Country
Date: Jan 23, 2000
>N63980, RV6A, O360, CSP just finished its 2ND X country Venice FL to PHX AZ >and back (Over 4,000 miles) total time on ACFT now 66 hrs. Other then Joe, I hope you went faster than 60.6 ml/hr (4000 ml -:- 66hrs)! Even my old Citrabira did better going from Colorado to Yukatan, Mexico. Maybe you could check your logs. We would be interested in some details like fuel burns, power settings and TAS. Got to go and sand filler around position lights so I can join you lucky flying gang. Do not archieve. Lothar |||-6A tip up; fuel and brake lines before starting canopy ||| Lakewood/ Denver, CO ________________________________________________________________________________
From: "Zeidman, Richard B" <Richard.Zeidman(at)PHL.Boeing.com>
Subject: FW: Equipment Location-RV6A
Date: Jan 23, 2000
> ---------- > From: Zeidman, Richard B > Sent: Sunday, January 23, 2000 10:15 AM > To:
'dmedema@physio-control.com' > Subject: Equipment Location-RV6A > Sensitivity: Private > > Doug, > I'm at the same spot in construction as you are. I ordered the drawing > OP-12 from Vans which shows the location of the electrical components for > their prefab wiring harness. I'm making my own harness, but I thought it > would be helpful to get that drawing ( and it was). > I'm putting my gascolator in the left wing root. In order to get it to > fit, I made a cardboard template of the left side of the fuse fwd of the > spar and fitted all of the parts and fuel lines onto it. That way the > holes in the side of the fuselage turn out in the right spot. Other than > that I'm following the standard drawings. > Good luck, > Rich Zeidman > RV6A 25224 > engine coming next month > ________________________________________________________________________________
Date: Jan 23, 2000
From: Finn Lassen <finnlassen(at)netzero.net>
Subject: Re: RMI Monitor Fuel Sensor
The only handling that I know of is to place the sensor before the pump. The theory I've just come up with is this: from the fuel pump onwards you have a solid column of non-compressible fuel under pressure - no matter how long the line between pump and sensor, any pulse transmitted by the pump instantaneously reaches the sensor. On the other hand, the column of fuel from the pump to the tank terminates in the softer, compressible air in the fuel tank, which acts as a damper. In the documentation that came with the sensor I bought from Matt there is a schematic of an electronic circuit that's supposed to eliminate false counts from the sensor caused by vibrations of the sensor. I couldn't easily get it to work and found it easier to more the sensor before the pump(s). Finn "John B. Holmgreen" wrote: > For those of you using the RMI fuel flow sensor......I experience an > increase of approximately 2 GPH fuel flow at cruise settings when I turn on > the electric fuel boost pump and it returns to what I compute as "normal" > fuel flow when I turn the boost pump off. > > Fuel pressure reads 6PSI (@6500 msl) with the engine driven pump and 7 > with the electric boost pump on. > > The sensor is mounted on the sidewall, just rear of the rudder pedals. > (RV-6A) The boost pump is mounted on the wing spar and I have about 20" of > tube with a very gradual 90 degree bend with about 6" of straight tube > length prior to the sensor. NetZero - Defenders of the Free World ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Do not lose heart. My first question to him would be what equipment was he using. Most are chadwick brand. There are 177, 192 , 2000 and 5800. There are also other brands, and they basically work the same. The chadwick people are very helpful and can be a help to your man getting him trained to use the equipment to it's best advantage. If he was not trained you cannot blame him. ( I did technical training so I can feel his pain). I would suggest finding a helicopter near you and ask the mechanic where they get balanced. They probably do it themselves. Compared to doing a helicopter a prop is incredibly easy. If they have not done a prop again a call to chadwik will give all the guidance they need. There is also a book put out by Chadwick called "smooth propellor" that has all the guidance necessary and is even considered approved data for balancing certified aircraft ( yes certified aircraft require a 337 for balance!). If you still have problems or questions reply as needed and I will help. I would do your prop but I am in Dallas. -----Original Message----- From: Larry Pardue <n5lp(at)carlsbad.net> Date: Saturday, January 22, 2000 11:26 PM Subject: Re: RV-List: Prop Balancing > > >> >>First. ips is inches per second which refers to accelerometers which >measure >>acceleration in distance.( there also are velometers which work off of >>velocity). The "ips" reading IS your amplitude, or more simply the strength >>of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable >>vibration) you have a lazy mechanic. > > >I certainly can not argue with you. It is apparent you know what you are >talking about. > >I went in thinking ips stood for inches per second and specifically asked >him. He said "interruptions per second" (I said I thought impulses per >second in my first post, but I have since remembered), which I must admit >did not make sense to me as .2 interruptions per second sounds really slow. >I also asked him about amplitude and he said his system does not measure it. >I expected the system to also measure phase and again he said no and that is >why the first placement is arbitrary. > > >>If washers are placed arbitrarily you >>again are dealing with a idiot. The system is simple. The accelerometer can >>only measure vibration in one plane, so it is pointed to the center of >crank >>in plane with prop and as close as possible to it. The accelerometer not >>only gives a strength reading but also a "phase angle" reading which sends >>the appropriate signal to the strobex flasher. Reflective tape is placed on >>prop ( I put a piece on each blade of different shape in case subject blade >>is where I could not see). When pointing the strobe at prop while running >>you note where tape is. Aircraft is shut down and the prop put back where >>you saw it. Here is the simple fact. The accelerometer ALWAYS wants the >>wieght put accross from it since the accelerometer is signaling a flash >when >>heavy part is NEXT to it. > >My mechanic had a strobe system but said he does not normally use it. He >said he does use it to detect dynamic tracking problems. > >>So you put some weight accross from where the >>accelerometer is (when blade is as observed with flash) and aircraft run >>again. If you were .4 and now are .2 and blade is in same place as before, >>you only added 1/2 of amount necessary. I do not stop until I get the >lowest >>reading. The newer equipment also mounts a accelerometer back on the >>accessory case. Reason is if vibration here gets better as prop gets better >>you are ok. If case gets worse as prop gets better, you have problems other >>than prop. Bent crank or other items. I want to make it clear I do not want >>to flame you, but vibration and the methods to control it are serious and I >>want people to understand this. Oh yeah, I know this from 20 years of doing >>this on helicopters ( lots of rotating stuff!). Bill N. RV4 flying. >>PPSEL.A&P-IA, Chief Inspector and many other things not as intresting. > > >Thanks for all the good info. I am at kind of a loss as to what to do. > >I flew 500 miles up and back to the big city area to a highly recommended >prop guy with a lot of experience only to find out he is an "idiot." >Sometimes I feel like I can't win on this deal. I get pieces breaking and >many people recommend balancing although the airplane feels smooth. I ask >around and go to the professional who is recommended and get reports he is >doing a bad job. Others say even if I am balanced vibrations of a different >frequency will break my parts. On my professional paint job I know I got a >bad job. I get my car oil changed and they put the wrong fluids in the >wrong holes and break the aircleaner. > >There are a lot of things I am not capable of doing. If I can't go to the >recommended professionals, I don't know what to do. > >Larry Pardue >Carlsbad, NM > >RV-6 N441LP >http://www.carlsbadnm.com/n5lp/index.htm > > ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Amen! -----Original Message----- From: Sam Buchanan <sbuc(at)hiwaay.net> Date: Saturday, January 22, 2000 11:27 PM Subject: Re: RV-List: Prop Balancing > > >Larry Pardue wrote: >> >> >> Listers, >> >> Brian Denk and I both took our RVs to New Mexico Aircraft Propeller in Belen >> NM today to get them dynamically balanced. I found it very interesting >> although David, the owner said "it isn't rocket science." >> >> For those of you that haven't seen this I will give a brief summary: Take >> top cowl off engine and attach vibration sensor to engine with cables >> running out to the display unit. Run engine at full power (in our case, and >> in our case with Sensenich 72FM8 props and O-360s it was 2130 RPM at 5300 >> MSL and about 60 degrees) while vibration is read. The vibration is given >> in ips, which I believe he said is impulses per second. No amplitude is >> measured. If the vibration is below .2 ips nothing is done, if it is higher >> washers are screwed temporarily to the spinner using spinner mounting >> screws. These weights are put at an arbitrary location as there is no phase >> detection either. If the vibration is worse on the next run the weights are >> moved 180 degrees, if it is better the weights are fine tuned by trial and >> error. When a final location is determined a bit more weight is added and >> then all the weights are moved inboard to the spinner bulkhead where they >> are secured with a bolt and nut through a newly drilled hole. The bit more >> weight is because of the move inboard. >> >> Whenever I have posted about the breaking of cowl mount hinges and exhaust >> supports people have e-mailed me about getting the prop balanced. I think >> that is a good response, but I have always felt it was quite smooth. I have >> also gotten e-mail indicating 72FM8 props are delivered out of balance. >> Well, to put it to rest I had to have it balanced. >> >> The facts in this case. Brian Denk's vibration was at .1 ips or below. As >> smooth as it comes according to the prop guy. Smoother than a lot of >> turboprops. The lucky SOB! He still notes his fire extinguisher trembling >> a bit though. >> >> My vibration was about .4 ips. Quite smooth but at a level where it can be >> improved. He got mine to between .1 and .2 ips. I think I can tell a >> difference in flight, but probably could not swear to it on a stack of >> Bibles. >> >> Any further breakage, at least I will know it is not vibration. >> >> Larry Pardue >> Carlsbad, NM >> >> RV-6 N441LP > > >I am a bit perplexed by Larry's description of his prop balance >technician placing weights by "trial and error"! The tech that balanced >the prop on 399SB used a system that left very little to chance. If you >wish to see more info and photos about this system, you can go here: > >http://home.HiWAAY.net/~sbuc/journal/airport5.html > >I found that .4 inches per second was pretty rough. The prop on my RV-6 >was brought down to 0.06 ips, and it is still not as smooth as some of >the other RV's in the area. > >However way you cut it though, dynamic prop balancing is a very good >thing! > >Sam Buchanan >"The RV Journal" http;//home/hiwaay.net/~sbuc/journal > > ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
> >First. ips is inches per second which refers to accelerometers which >measure > >acceleration in distance.( there also are velometers which work off of > >velocity). The "ips" reading IS your amplitude, or more simply the >strength > >of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable > >vibration) you have a lazy mechanic. > > >I certainly can not argue with you. It is apparent you know what you are >talking about. > > >Thanks for all the good info. I am at kind of a loss as to what to do. > >I flew 500 miles up and back to the big city area to a highly recommended >prop guy with a lot of experience only to find out he is an "idiot." >Sometimes I feel like I can't win on this deal. I get pieces breaking and >many people recommend balancing although the airplane feels smooth. I ask >around and go to the professional who is recommended and get reports he is >doing a bad job. Others say even if I am balanced vibrations of a >different >frequency will break my parts. On my professional paint job I know I got a >bad job. I get my car oil changed and they put the wrong fluids in the >wrong holes and break the aircleaner. > >There are a lot of things I am not capable of doing. If I can't go to the >recommended professionals, I don't know what to do. > >Larry Pardue >Carlsbad, NM > >RV-6 N441LP Well guys, since I'm the other guy in this episode, I might as well jump into the fray. This prop guy was also recommended to me by a very trusted A&P/IA friend of mine who knows of this guy's integrity and abilities. Since his equipment indicated .1 ips on my plane, he could only offer that he felt it was fine and then asked me what I believed was a fair price to pay. We agreed to $50 and that was it. If it weren't for the fact that my fire extinguisher tends to wobble around at certain power settings, I wouldn't have even thought about getting the dynamic balance done. Nothing in the cowling has broken after 22 hours, and there are no uncomfortable resonances or pulses that I can feel anywhere in the cabin. Lycoming engines shake, rattle and roll, and that's just the way it is. Watching Larry fire up his plane during his testing with the cowl top off certainly confirms how much these things move around during startup and shut down! Yikes...no wonder stuff breaks in there. I know mine does the same thing, but I just haven't ever been outside the plane to see it happen. I may redo the test after everything is painted (spinner) and the engine/airframe has more time on it. I mean, everything is so new and it has to take some time for things to settle in, especially the engine mounts. I will probably have another person do the next test, perhaps a guy I met at work who does balancing on our HVAC fans. Or, the maintenance operation at my airport might get the call...no doubt for MUCH more money. We simply went with the advice of trusted friends of ours and sometimes things don't go as originally intended. Everyone has his/her different views on what defines quality and value in services rendered. Oh well, just one more "AFLE" in life. (AFLE=another f**& *# learning experience). Brian Denk RV8 N94BD ________________________________________________________________________________
From: "John" <fasching(at)amigo.net>
Subject: Prop Balancing
Date: Jan 23, 2000
Here's a naive question... (I'm out of my area of knowledge here!) The posts re prop balancing all seem to be on planes with metal props. Does this balancing also work on wooden props with the same techniques and equipment? It would seem so to me, but most of you folks talking about your balancing seem to have metal props. Advise? RV-6A w/Warnke wooden prop ________________________________________________________________________________
Date: Jan 23, 2000
From: The Razers <razer(at)midwest.net>
Subject: Prop Balancing
Anybody care to comment about balancing a wood prop when a Landoll Balancer is also installed. chet ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Funny, I didn't receive a 337 when I got my prop balanced by a local Large FBO. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Bill Noel <bnoel(at)ausa.net> Date: Sunday, January 23, 2000 10:18 AM Subject: Re: RV-List: Prop Balancing > >Do not lose heart. My first question to him would be what equipment was he >using. Most are chadwick brand. There are 177, 192 , 2000 and 5800. There >are also other brands, and they basically work the same. The chadwick people >are very helpful and can be a help to your man getting him trained to use >the equipment to it's best advantage. If he was not trained you cannot blame >him. ( I did technical training so I can feel his pain). I would suggest >finding a helicopter near you and ask the mechanic where they get balanced. >They probably do it themselves. Compared to doing a helicopter a prop is >incredibly easy. If they have not done a prop again a call to chadwik will >give all the guidance they need. There is also a book put out by Chadwick >called "smooth propellor" that has all the guidance necessary and is even >considered approved data for balancing certified aircraft ( yes certified >aircraft require a 337 for balance!). If you still have problems or >questions reply as needed and I will help. I would do your prop but I am in >Dallas. >-----Original Message----- >From: Larry Pardue <n5lp(at)carlsbad.net> >To: rv-list(at)matronics.com >Date: Saturday, January 22, 2000 11:26 PM >Subject: Re: RV-List: Prop Balancing > > >> >> >>> >>>First. ips is inches per second which refers to accelerometers which >>measure >>>acceleration in distance.( there also are velometers which work off of >>>velocity). The "ips" reading IS your amplitude, or more simply the >strength >>>of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable >>>vibration) you have a lazy mechanic. >> >> >>I certainly can not argue with you. It is apparent you know what you are >>talking about. >> >>I went in thinking ips stood for inches per second and specifically asked >>him. He said "interruptions per second" (I said I thought impulses per >>second in my first post, but I have since remembered), which I must admit >>did not make sense to me as .2 interruptions per second sounds really slow. >>I also asked him about amplitude and he said his system does not measure >it. >>I expected the system to also measure phase and again he said no and that >is >>why the first placement is arbitrary. >> >> >>>If washers are placed arbitrarily you >>>again are dealing with a idiot. The system is simple. The accelerometer >can >>>only measure vibration in one plane, so it is pointed to the center of >>crank >>>in plane with prop and as close as possible to it. The accelerometer not >>>only gives a strength reading but also a "phase angle" reading which sends >>>the appropriate signal to the strobex flasher. Reflective tape is placed >on >>>prop ( I put a piece on each blade of different shape in case subject >blade >>>is where I could not see). When pointing the strobe at prop while running >>>you note where tape is. Aircraft is shut down and the prop put back where >>>you saw it. Here is the simple fact. The accelerometer ALWAYS wants the >>>wieght put accross from it since the accelerometer is signaling a flash >>when >>>heavy part is NEXT to it. >> >>My mechanic had a strobe system but said he does not normally use it. He >>said he does use it to detect dynamic tracking problems. >> >>>So you put some weight accross from where the >>>accelerometer is (when blade is as observed with flash) and aircraft run >>>again. If you were .4 and now are .2 and blade is in same place as before, >>>you only added 1/2 of amount necessary. I do not stop until I get the >>lowest >>>reading. The newer equipment also mounts a accelerometer back on the >>>accessory case. Reason is if vibration here gets better as prop gets >better >>>you are ok. If case gets worse as prop gets better, you have problems >other >>>than prop. Bent crank or other items. I want to make it clear I do not >want >>>to flame you, but vibration and the methods to control it are serious and >I >>>want people to understand this. Oh yeah, I know this from 20 years of >doing >>>this on helicopters ( lots of rotating stuff!). Bill N. RV4 flying. >>>PPSEL.A&P-IA, Chief Inspector and many other things not as intresting. >> >> >>Thanks for all the good info. I am at kind of a loss as to what to do. >> >>I flew 500 miles up and back to the big city area to a highly recommended >>prop guy with a lot of experience only to find out he is an "idiot." >>Sometimes I feel like I can't win on this deal. I get pieces breaking and >>many people recommend balancing although the airplane feels smooth. I ask >>around and go to the professional who is recommended and get reports he is >>doing a bad job. Others say even if I am balanced vibrations of a >different >>frequency will break my parts. On my professional paint job I know I got a >>bad job. I get my car oil changed and they put the wrong fluids in the >>wrong holes and break the aircleaner. >> >>There are a lot of things I am not capable of doing. If I can't go to the >>recommended professionals, I don't know what to do. >> >>Larry Pardue >>Carlsbad, NM >> >>RV-6 N441LP >>http://www.carlsbadnm.com/n5lp/index.htm >> >> > > ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
I had it done on a wood bladed Aeromatic prop. The one with the black blades that change pitch due to air loads and centrifugal forces. Worked very well. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: John <fasching(at)amigo.net> Date: Sunday, January 23, 2000 11:20 AM Subject: RV-List: Prop Balancing > >Here's a naive question... (I'm out of my area of knowledge here!) > >The posts re prop balancing all seem to be on planes with metal props. Does >this balancing also work on wooden props with the same techniques and >equipment? It would seem so to me, but most of you folks talking about your >balancing seem to have metal props. Advise? >RV-6A w/Warnke wooden prop > > ________________________________________________________________________________
From: TCRV6(at)aol.com
Date: Jan 23, 2000
Subject: wing walk doubler-help-rv6
does the wing walk skin slip under the main wing spar aft.flange or does it butt up flush with the aft. main spar flange. tcrv6(at)aol.com left-wing ________________________________________________________________________________
Date: Jan 23, 2000
From: Hal Kempthorne <kempthorne(at)earthlink.net>
Subject: Re: Engine Baffles responses
> >all 4 cylinders on every engine should be the same regardless of model. While I would be more suspect of the accuracy of the baffle parts, I would not be willing to completely rule out differences in engines -- even differences in two engines of the same model. This would apply even more if they had been overhauled. Tolerances, tolerances, tolerances again! I wonder how Lycoming determines where to put the holes and what the tolerances are. I wonder if they make the cylinders? I wonder if there are more than one drilling setup? I wonder if they worry much about the locations of these holes they never use? Anyone have an engine apart and willing to measure how cylinders compare if installed in the same place in the case? Mine baffle parts were not off by much on a new 0360A1A from Van. I can find reasons to complain about the documentation but I can do that with most any docs I see. What really helps construction are some good photos or better, the real thing in the next hangar. I'm about to install the baffle seal fabric. I am trying to think of easy way to determine if metal parts need to be trimmed further. One suggestion involved cardboard fingers. I was also thinking of blobs of clay. I almost think it would be easier to make a full pressure plenum or whatever it is called (where the cowl is not part of the pressure chamber). Hal Kempthorne - SJC RV6a N7HK at SCK Hangar K3 Debonair N6134V for sale ________________________________________________________________________________
From: "Alex Peterson" <alexpeterson(at)usjet.net>
Subject: Cooling inlet clearance
Date: Jan 23, 2000
For those of you with RV6's with C/S 360's and epoxy cowlings: About how much clearance is there between the #1 cylinder fins (the largest ones) and the epoxy inlet ramp which is bonded to the upper cowl? I simply fit the epoxy ramps on the top cowl by best fit, but there is only about 3/4" clearance at the minimum point, which doesn't seem to be much. I could move the ramp forward, but wanted to know if others who are flying might comment. Alex Peterson Maple Grove, MN 6A ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)mari.net>
Subject: Re: wing walk doubler-help-rv6
Date: Jan 23, 2000
Hi: The wing walk doubler should butt up to the flange of the spar. Been there....doin' it again. Regards, Jeff Orear RV6A 25171 second wing Peshtigo, WI -----Original Message----- From: TCRV6(at)aol.com <TCRV6(at)aol.com> Date: Sunday, January 23, 2000 12:01 PM Subject: RV-List: wing walk doubler-help-rv6 > > > does the wing walk skin slip under the main wing spar aft.flange or >does it butt up flush with the aft. main spar flange. > > tcrv6(at)aol.com left-wing > > ________________________________________________________________________________
From: "John B. Holmgreen" <j32619(at)innova.net>
Subject: Re: RMI Monitor Fuel Sensor
Date: Jan 23, 2000
Thanks Karl and others that have replied. From the suggestions I have received, I believe the solution may be to reverse the positions of the fuel sensor and the electric boost pump. Then I may be able to enter one K-Factor that will work in both situations. In this case all fuel will be pulled through the sensor rather than pulled by the engine driven pump and pushed by the electric pump. Sound reasonable? John ----- Original Message ----- Subject: Re: RV-List: RMI Monitor Fuel Sensor > > I also get a higher reading of fuelflow with the electric pump on .I think > this problem was discussed on the list some time ago.The higher reading is > apparently caused by the pressure pulses generated by the boost > pump... > RV6AQ VH-KHA 31 Hours > KARL AHAMER NSW AUSTRALIA > ASCOT(at)HINET.NET.AU > > ________________________________________________________________________________
Date: Jan 23, 2000
From: Arthur Glaser <airplane(at)megsinet.net>
Subject: Re: Prop Balancing
John wrote: > > Here's a naive question... (I'm out of my area of knowledge here!) > > The posts re prop balancing all seem to be on planes with metal props. Does > this balancing also work on wooden props with the same techniques and > equipment? It would seem so to me, but most of you folks talking about your > balancing seem to have metal props. Advise? > RV-6A w/Warnke wooden prop Wood props will change in mass due to humidity. The balance may not last. They are also considered to be inherently smoother. This may be why the above is true. ________________________________________________________________________________
Date: Jan 23, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Electroair ignition
> >Great Bob, thanks a bunch, this is what I was looking for. So I could >wire it to the battery side of my essential bus switch...the one that >connects the e-bus to the battery direct??? Or better yet, right from the hot side of the battery contactor. This makes the ignition system feed totally independent of any other system wiring. >Jeff calls for shielded >conductor for noise, do you see this as necessary? I don't think shielding is needed for this system. Shielded wire is for a very specific kind of noise elimination that I don't think exists on this product. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
Date: Jan 23, 2000
From: George McNutt <gmcnutt(at)intergate.bc.ca>
Subject: Re: Accesories & Instrument Panel
Thanks to all who responded both on & off List to my question about the small screws and nuts holding the electric trim switch/LED indicator/ELT monitor etc to the instrument panel. Here is a summary of the answers recieved both on and off the List. 1) Yes it definitely is a problem trying to remove & reinstall # 2 nuts for maintenance at some later date, those little guys are hard to handle and vanish when you drop them! 2) If you have not already drilled the holes in your panel, tap the instrument panel with a #2 or #4 tap as appropriate. If unable to find a #2 tap some builders are useing sheet metal screws directly into the instrument panel. ("The little sheetmetal screws we used to mount the servos in our models are just the right size (#2?) for attaching these small items"). 3) If you have already drilled the mounting holes in the panel for the #2 screws,[or #4] and they are oversize for tapping, cut a small strip of aluminum same thickness as panel, apply JB Weld and stick it to the back of the panel over the through holes. You can then drill and tap to appropriate size.[after the JB sets up.] 4) Riv-nuts and nut plates are reported to be available in a #4-40 size but I have not been able to find any locally. George McNutt 6-A inst-pnl Langley, B.C. ________________________________________________________________________________
Date: Jan 23, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Breaker/switch orientation
> >Electrical gurus, > >I have now arrived at my final panel layout (RV-8) and cut all of the holes, >so I'm committed. The bottom of the panel features a row of Potter-Brumfield >W23 series breakers and W31 series switch/breakers for most major functions. >These will have their input terminals connected with a piece of copper strip >for low voltage loss and good mechanical integrity... very standard >practice. The problem however is that in using a combination of the pullable >breakers and switch/breakers I find that the two terminals on each style >have opposite functions. On the breakers the top terminal is labeled "line" >and the bottom terminal "load". The switch/breakers are labeled in an >opposite manner. Needless to say it would be far simpler to simply run my >copper bus strip across the top, but then the switch/breakers would be then >be wired in opposite fashion t thier labeling. My question is this: does it >matter? I don't know what's inside of there, so if anyone has a clue why >those switch/breakers couldn't be used in an opposite manner I'd appreciate >knowing about it. Electric Bob? it's not critical . . . there are some very small considerations for internal construction of breakers and switches with respect to line and load terminals . . . that come into play only when a breaker is required to operate. Repeat after me, "MY airplane will be totally free of nuisance trips." . . . you you can wire the breakers any way you like. Why not make it simpler yet and buy your bus bars and circuit protection already assembled and installed in 10 minutes? The breaker-patch in airplanes needs to go away . . . it only adds weight, costs dollars, uses up panel space, takes hours to build, and adds no value in terms of operability or flight safety over a simple fuse panel. . . . it DOES look sexy tho . . . Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
Date: Jan 24, 2000
From: "Builder's Bookstore" <winterland(at)rkymtnhi.com>
Subject: Re: Electroair ignition
Bob, Whats the status of Revision-9? When do you think they might be ready to ship? Any price changes? I've got 4 copies of R-8 left Andy Builder's Bookstore (Lancair Bookstore; Glastar Bookstore, AMT On-Line Bookstore, Cleaveland Aircraft Tools Bookstore) ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
It works on anything that spins. I have tracked and balanced all my ceiling fans! -----Original Message----- From: John <fasching(at)amigo.net> Date: Sunday, January 23, 2000 10:54 AM Subject: RV-List: Prop Balancing > >Here's a naive question... (I'm out of my area of knowledge here!) > >The posts re prop balancing all seem to be on planes with metal props. Does >this balancing also work on wooden props with the same techniques and >equipment? It would seem so to me, but most of you folks talking about your >balancing seem to have metal props. Advise? >RV-6A w/Warnke wooden prop > > ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Many do not know, look into FAR43 appendix on Major repairs/alterations props. Changing the balance of a prop is a major. If you ask for Chadwicks copy of "smooth Propellor" they have on cover the letter from FAA region considering that book approved data for modifying a propellor balance by adding weights. Approved data is not necessary if it is a minor. Unfortunately since the FAA rarely inforces many of A&P infractions we assume we are right. Study the regs, call FAA region, not your local guy and you may be suprised what you find. -----Original Message----- From: Cy Galley <cgalley(at)accessus.net> Date: Sunday, January 23, 2000 11:17 AM Subject: Re: RV-List: Prop Balancing > >Funny, I didn't receive a 337 when I got my prop balanced by a local Large >FBO. > >Cy Galley - Editor, B-C Contact! >(Click here to visit our Club site at http://www.bellanca-championclub.com) > > >-----Original Message----- >From: Bill Noel <bnoel(at)ausa.net> >To: rv-list(at)matronics.com >Date: Sunday, January 23, 2000 10:18 AM >Subject: Re: RV-List: Prop Balancing > > >> >>Do not lose heart. My first question to him would be what equipment was he >>using. Most are chadwick brand. There are 177, 192 , 2000 and 5800. There >>are also other brands, and they basically work the same. The chadwick >people >>are very helpful and can be a help to your man getting him trained to use >>the equipment to it's best advantage. If he was not trained you cannot >blame >>him. ( I did technical training so I can feel his pain). I would suggest >>finding a helicopter near you and ask the mechanic where they get balanced. >>They probably do it themselves. Compared to doing a helicopter a prop is >>incredibly easy. If they have not done a prop again a call to chadwik will >>give all the guidance they need. There is also a book put out by Chadwick >>called "smooth propellor" that has all the guidance necessary and is even >>considered approved data for balancing certified aircraft ( yes certified >>aircraft require a 337 for balance!). If you still have problems or >>questions reply as needed and I will help. I would do your prop but I am in >>Dallas. >>-----Original Message----- >>From: Larry Pardue <n5lp(at)carlsbad.net> >>To: rv-list(at)matronics.com >>Date: Saturday, January 22, 2000 11:26 PM >>Subject: Re: RV-List: Prop Balancing >> >> >>> >>> >>>> >>>>First. ips is inches per second which refers to accelerometers which >>>measure >>>>acceleration in distance.( there also are velometers which work off of >>>>velocity). The "ips" reading IS your amplitude, or more simply the >>strength >>>>of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable >>>>vibration) you have a lazy mechanic. >>> >>> >>>I certainly can not argue with you. It is apparent you know what you are >>>talking about. >>> >>>I went in thinking ips stood for inches per second and specifically asked >>>him. He said "interruptions per second" (I said I thought impulses per >>>second in my first post, but I have since remembered), which I must admit >>>did not make sense to me as .2 interruptions per second sounds really >slow. >>>I also asked him about amplitude and he said his system does not measure >>it. >>>I expected the system to also measure phase and again he said no and that >>is >>>why the first placement is arbitrary. >>> >>> >>>>If washers are placed arbitrarily you >>>>again are dealing with a idiot. The system is simple. The accelerometer >>can >>>>only measure vibration in one plane, so it is pointed to the center of >>>crank >>>>in plane with prop and as close as possible to it. The accelerometer not >>>>only gives a strength reading but also a "phase angle" reading which >sends >>>>the appropriate signal to the strobex flasher. Reflective tape is placed >>on >>>>prop ( I put a piece on each blade of different shape in case subject >> ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Is that a harmonic balancer? It is best to balance prop without harmonic first, then install harmonic being sure the prop goes back in same place. The reason is the harmonic balancer reduces chances of DIFFERENT vibrations coming together with distructive results. Anything you do to reduce the vibrations in the first place helps. -----Original Message----- From: The Razers <razer(at)midwest.net> Date: Sunday, January 23, 2000 11:07 AM Subject: RV-List: Prop Balancing > >Anybody care to comment about balancing a wood prop when a Landoll >Balancer is also installed. > >chet > > blade >>>>is where I could not see). When pointing the strobe at prop while running >>>>you note where tape is. Aircraft is shut down and the prop put back where >>>>you saw it. Here is the simple fact. The accelerometer ALWAYS wants the >>>>wieght put accross from it since the accelerometer is signaling a flash >>>when >>>>heavy part is NEXT to it. >>> >>>My mechanic had a strobe system but said he does not normally use it. He >>>said he does use it to detect dynamic tracking problems. >>> >>>>So you put some weight accross from where the >>>>accelerometer is (when blade is as observed with flash) and aircraft run >>>>again. If you were .4 and now are .2 and blade is in same place as >before, >>>>you only added 1/2 of amount necessary. I do not stop until I get the >>>lowest >>>>reading. The newer equipment also mounts a accelerometer back on the >>>>accessory case. Reason is if vibration here gets better as prop gets >>better >>>>you are ok. If case gets worse as prop gets better, you have problems >>other >>>>than prop. Bent crank or other items. I want to make it clear I do not >>want >>>>to flame you, but vibration and the methods to control it are serious and >>I >>>>want people to understand this. Oh yeah, I know this from 20 years of >>doing >>>>this on helicopters ( lots of rotating stuff!). Bill N. RV4 flying. >>>>PPSEL.A&P-IA, Chief Inspector and many other things not as intresting. >>> >>> >>>Thanks for all the good info. I am at kind of a loss as to what to do. >>> >>>I flew 500 miles up and back to the big city area to a highly recommended >>>prop guy with a lot of experience only to find out he is an "idiot." >>>Sometimes I feel like I can't win on this deal. I get pieces breaking and >>>many people recommend balancing although the airplane feels smooth. I ask >>>around and go to the professional who is recommended and get reports he is >>>doing a bad job. Others say even if I am balanced vibrations of a >>different >>>frequency will break my parts. On my professional paint job I know I got >a >>>bad job. I get my car oil changed and they put the wrong fluids in the >>>wrong holes and break the aircleaner. >>> >>>There are a lot of things I am not capable of doing. If I can't go to the >>>recommended professionals, I don't know what to do. >>> >>>Larry Pardue >>>Carlsbad, NM >>> >>>RV-6 N441LP >>>http://www.carlsbadnm.com/n5lp/index.htm >>> >>> >> >> > > ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
.1 is a good balance and hench your aircraft is doing better. Remember there is more than just prop vibes as well. Someone who knows the equipment can scan the range of frequencys looking for the highest strength and compare to known rpms of other components and find other items at fault.(this is an awesome diagnostic tool!) If someone refers you to a guy it is not your fault. As I mentioned before, this guy just may need some training, this dosen't come naturally even though it is not inherently difficult. It has to be something you enjoy and then experience counts for alot too. In fairness I have balanced more main& tail rotors than I could count, and had some real head scratchers too! Lucky for you prop balancing is much easier. The dynamics of vibration are very intresting, but the fact is vibration kills. Keep your head up, most A&P's are NOT crooks and have the highest standards, the real reason for safety in this industry. -----Original Message----- From: Brian Denk <akroguy(at)hotmail.com> Date: Sunday, January 23, 2000 10:10 AM Subject: Re: RV-List: Prop Balancing > > >> >First. ips is inches per second which refers to accelerometers which >>measure >> >acceleration in distance.( there also are velometers which work off of >> >velocity). The "ips" reading IS your amplitude, or more simply the >>strength >> >of your vibration. If nothing is done at .2 ips ( the HIGHEST acceptable >> >vibration) you have a lazy mechanic. >> >> >>I certainly can not argue with you. It is apparent you know what you are >>talking about. > >> >> >>Thanks for all the good info. I am at kind of a loss as to what to do. >> >>I flew 500 miles up and back to the big city area to a highly recommended >>prop guy with a lot of experience only to find out he is an "idiot." >>Sometimes I feel like I can't win on this deal. I get pieces breaking and >>many people recommend balancing although the airplane feels smooth. I ask >>around and go to the professional who is recommended and get reports he is >>doing a bad job. Others say even if I am balanced vibrations of a >>different >>frequency will break my parts. On my professional paint job I know I got a >>bad job. I get my car oil changed and they put the wrong fluids in the >>wrong holes and break the aircleaner. >> >>There are a lot of things I am not capable of doing. If I can't go to the >>recommended professionals, I don't know what to do. >> >>Larry Pardue >>Carlsbad, NM >> >>RV-6 N441LP > > >Well guys, since I'm the other guy in this episode, I might as well jump >into the fray. This prop guy was also recommended to me by a very trusted >A&P/IA friend of mine who knows of this guy's integrity and abilities. >Since his equipment indicated .1 ips on my plane, he could only offer that >he felt it was fine and then asked me what I believed was a fair price to >pay. We agreed to $50 and that was it. If it weren't for the fact that my >fire extinguisher tends to wobble around at certain power settings, I >wouldn't have even thought about getting the dynamic balance done. Nothing >in the cowling has broken after 22 hours, and there are no uncomfortable >resonances or pulses that I can feel anywhere in the cabin. > >Lycoming engines shake, rattle and roll, and that's just the way it is. >Watching Larry fire up his plane during his testing with the cowl top off >certainly confirms how much these things move around during startup and shut >down! Yikes...no wonder stuff breaks in there. I know mine does the same >thing, but I just haven't ever been outside the plane to see it happen. > >I may redo the test after everything is painted (spinner) and the >engine/airframe has more time on it. I mean, everything is so new and it >has to take some time for things to settle in, especially the engine mounts. > I will probably have another person do the next test, perhaps a guy I met >at work who does balancing on our HVAC fans. Or, the maintenance operation >at my airport might get the call...no doubt for MUCH more money. > >We simply went with the advice of trusted friends of ours and sometimes >things don't go as originally intended. Everyone has his/her different views >on what defines quality and value in services rendered. Oh well, just one >more "AFLE" in life. (AFLE=another f**& *# learning experience). > >Brian Denk >RV8 N94BD > > ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 23, 2000
Wood props are smoother due to the charachteristics of the wood, it gives thus damping vibration somewhat. To illustrate, get a piece of 2x4 and hit with hammer, then do same to solid piece os steel same size. Wood damps, metal transmits. -----Original Message----- From: Arthur Glaser <airplane(at)megsinet.net> Date: Sunday, January 23, 2000 1:25 PM Subject: Re: RV-List: Prop Balancing > > >John wrote: > >> >> Here's a naive question... (I'm out of my area of knowledge here!) >> >> The posts re prop balancing all seem to be on planes with metal props. Does >> this balancing also work on wooden props with the same techniques and >> equipment? It would seem so to me, but most of you folks talking about your >> balancing seem to have metal props. Advise? >> RV-6A w/Warnke wooden prop > >Wood props will change in mass due to humidity. The balance may not last. >They are also considered to be inherently smoother. This may be why the above >is true. > > ________________________________________________________________________________
From: "Joe Wiza" <planejoe(at)ewol.com>
Subject: Re: Cross Country
Date: Jan 23, 2000
(total time on acft now 66hrs)(tirp time aprox 20 hrs) Didn't keep track of fuel burn and it probably wasn't to good because I run at full 75% power on x country. do not archieve ----- Original Message ----- From: Lothar Klingmuller <lothark(at)worldnet.att.net> Sent: Sunday, January 23, 2000 9:48 AM Subject: Re: RV-List: Cross Country > > >N63980, RV6A, O360, CSP just finished its 2ND X country Venice FL to PHX AZ > >and back (Over 4,000 miles) total time on ACFT now 66 hrs. Other then > > Joe, I hope you went faster than 60.6 ml/hr (4000 ml -:- 66hrs)! Even my > old Citrabira did better going from Colorado to Yukatan, Mexico. > Maybe you could check your logs. We would be interested in some details > like fuel burns, power settings and TAS. > Got to go and sand filler around position lights so I can join you lucky > flying gang. > > Do not archieve. > > Lothar |||-6A tip up; fuel and brake lines before starting canopy ||| > Lakewood/ Denver, CO > > ________________________________________________________________________________
From: "Tim Lewis" <timrv6a(at)earthlink.net>
Date: Jan 23, 2000
Subject: Re: RMI Monitor Fuel Sensor
>From the suggestions I have received, I believe the solution may be to > reverse the positions of the fuel sensor and the electric boost pump. > Then I may be able to enter one K-Factor that will work in both > situations. In this case all fuel will be pulled through the sensor rather > than pulled by the engine driven pump and pushed by the electric pump. > > Sound reasonable? My fuel flow sensor is before both the electric pump and the engine driven pump, and I still get the behavior that's being discussed (higher indicated flow rate when boost pump is on). Tim ****** Tim Lewis -- Springfield VA RV-6A N47TD - First Flight 18 Dec 99 TimRV6A(at)earthlink.net http://www.geocities.com/timrv6a ________________________________________________________________________________
Date: Jan 23, 2000
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: Prop Balancing
> >Anybody care to comment about balancing a wood prop when a Landoll >Balancer is also installed. > >chet Chet, I had my wood prop balanced with the Landoll harmonic balancer installed. Later, I removed the blalancer and flew the airplane for awhile. I didn't notice any change in vibration. That doesn't mean the Chadwick machine would not have noticed a change in vibration levels. If I was to install another wood prop and needed the weight forward, I believe I would install the "weight ring" (no moving parts). It is considerablly cheaper than the harmonic dampner. I would then have the prop dynamically balanced. Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 ________________________________________________________________________________
Date: Jan 23, 2000
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: Prop Balancing
> >Here's a naive question... (I'm out of my area of knowledge here!) > >The posts re prop balancing all seem to be on planes with metal props. Does >this balancing also work on wooden props with the same techniques and >equipment? It would seem so to me, but most of you folks talking about your >balancing seem to have metal props. Advise? >RV-6A w/Warnke wooden prop John, I balanced my wood prop and it did help the smoothness and was worthwhile, IMO. The improvement was much more dramatic on the Sensenich metal prop. I lucked out. Both the wood and metal props were balanced for free by a helicopter mechanic friend who was also a RV6 owner. I lent him my Croix when it was time to paint his plane. Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: Jan 23, 2000
Subject: Re: Breaker/switch orientation
In a message dated 1/23/00 1:09:14 PM Pacific Standard Time, nuckolls(at)aeroelectric.com writes: << The breaker-patch in airplanes needs to go away . . . it only adds weight, costs dollars, uses up panel space, takes hours to build, and adds no value in terms of operability or flight safety over a simple fuse panel. . . . it DOES look sexy tho >> Regarding sexy breakers, Carlingswitch <http://www.carlingswitch.com> has a new series of rocker switch breakers (rocker switch and breaker and in one) that look pretty swift. They are called their M-series breakers and are available in ratings up to 25A. I know that Wicks buys from Carlingswitch and they might be able to obtain these if you talk to their purchasing person. I bought some special Carlingswitch rocker switches that way a few years back. -GV ________________________________________________________________________________
From: "jkginth(at)swbell.net
by mta4.rcsntx.swbell.net (Sun Internet Mail Server sims.3.5.1999.09.16.21.57.p8) with ESMTP id" <0FOT00HVNLYAB1(at)mta4.rcsntx.swbell.net> for
Date: Jan 23, 2000
Subject: RV-9A Builders
Hello- I am looking for any 9A builders on the list that are working on the tail. Please contact me off list for some simple questions about required jigs. Thanks, John Ginther jkginth(at)swbell.net Wichita, KS (RV grin wanna be) ________________________________________________________________________________
From: "Russ Nichols" <russnichols(at)msn.com>
Subject: tube flaring w/ Rolo-flare tool
Date: Jan 23, 2000
I purchased the Rolo-flare tool from Cleveland. When I use it, the flare I produce isn't "centered". It gives me a nice surface in the tube, but one side of the tube doesn't flare out on the outside while the other has an extreme flare. I've never used one of these before, so I'm not sure if I'm doing something wrong. I double-checked the settings, but had no luck on numerous test pieces. Any suggestions? thanks, Russ Nichols RV-6 Tonia & Russell Nichols russnichols(at)msn.com ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: tube flaring w/ Rolo-flare tool
Date: Jan 23, 2000
>From: "Russ Nichols" <russnichols(at)msn.com> >Reply-To: rv-list(at)matronics.com >To: "RV List" >Subject: RV-List: tube flaring w/ Rolo-flare tool >Date: Sun, 23 Jan 2000 20:09:54 -0800 > > >I purchased the Rolo-flare tool from Cleveland. When I use it, the flare I >produce isn't "centered". It gives me a nice surface in the tube, but one >side of the tube doesn't flare out on the outside while the other has an >extreme flare. I've never used one of these before, so I'm not sure if I'm >doing something wrong. I double-checked the settings, but had no luck on >numerous test pieces. Any suggestions? > >thanks, > >Russ Nichols >RV-6 > >Tonia & Russell Nichols Russ, Did you use some lubricant on the tip of the male cone? A drop of oil or little dab of vaseline can make for a smoother flare. Also make sure the tubing is securely clamped in place so it can't twist or try to slide away from the cone as you crank it down into the tube. Not all of my flares look textbook perfect either, but they all sealed just fine. Just make sure there are no cracks or burrs, and the flare is as wide as the sleeve that nests up against it. I also burnish the flared end with a green scotchbrite pad before assembly. It just looks better that way. I've found that the real trick is to get the end of the tube as true and clean as possible before forming the flare. After cutting it to length, I carefully file the end flat and true, and debur the inside to remove the little lip of metal that is formed during the use of the tubing cutter. Yes, you will scrap a few pieces before you get the touch figured out, but that's just a typical learning curve to be negotiated. Keep at it and you'll do fine. Have fun. Brian Denk RV8 N94BD flying Brian Denk >russnichols(at)msn.com > > ________________________________________________________________________________
From: "Robert Burns" <hsierra(at)flash.net>
Subject: Re: tube flaring w/ Rolo-flare tool
Date: Jan 23, 2000
Make sure that you are cutting the end of the tube square. i use a tubing cutter instead of a saw. if the end is not square it will not flare uniformly. Robert Burns RV-4 s/n 3524 N82RB new pics on my web page www.flash.net/~hsierra >I purchased the Rolo-flare tool from Cleveland snip snip ________________________________________________________________________________
From: capsteve(at)wzrd.com
Subject: Re: Prop Balancing
Date: Jan 23, 2000
some of you guys seem to know a bunch about balancing, so i'm gonna ask about my cherokee. its a 62' 160 hp conical mount lycoming. i had it balanced by a local and he couldn't do it cause the "numbers" kept changing. its swinging a sensinich that was sent out to be staticly balanced. i seem to have a pretty good vibe but my mechanic insists the old conical mounts (system not rubber) were the culprit. the motor was just overhauled 60 hrs ago by pen yann. any ideas???? capsteve(at)wzrd.com Steve DiNieri ________________________________________________________________________________
Date: Jan 23, 2000
From: Bob Skinner <bskinner(at)vcn.com>
Subject: Re: tube flaring w/ Rolo-flare tool
I cut the tubing on the band saw. I then go to the 6" Scotchbrite wheel to remove the heavy burrs and then slide on a sleeve, backwards. I then use the end of the sleeve to check for "square" and touch up as necessary on the Scotchbrite wheel (gray, fine wheel). I also use a fine file or sometimes a pocket knife to clean out any burrs on the inside of the tubing. Oh, don't forget to turn the sleeve around before flaring:) Bob Skinner Buffalo, WY (1995 RV6 sold after 4 years & 470 hrs) EAA Tech Counselor # 3726 ________________________________________________________________________________
From: "D. F. Cimperman, Jr." <cimperman(at)tusco.net>
Subject: Flight Instructor Needed
Date: Jan 24, 2000
I am a Student Pilot. I have over 40 hours in a 150, but I have not flown in over 2 years. I need an Instructor in the New Philadelphia Ohio Area to help (South Of Akron/Canton Ohio). If you have an RV6A that would be even better. Thanks for any assistance. Dave Cimperman(at)Tusco.Net DFC2(at)Hotmail.Com D. F. Cimperman, Jr. ICQ 44164614 AOL IM "DFCimp" ________________________________________________________________________________
Date: Jan 23, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Re: Prop Balancing
> > some of you guys seem to know a bunch about > balancing, so i'm gonna ask > about my cherokee. its a 62' 160 hp conical mount > lycoming. i had it > balanced by a local and he couldn't do it cause the > "numbers" kept changing. > its swinging a sensinich that was sent out to be > staticly balanced. i seem > to have a pretty good vibe but my mechanic insists > the old conical mounts > (system not rubber) were the culprit. the motor was > just overhauled 60 hrs > ago by pen yann. > > any ideas???? > capsteve(at)wzrd.com > Steve DiNieri > If there is something wrong with an accessory or other rotating part of the engine, the prop balance will give a reading like you are having. I have a CONICAL mount O-320 B2B that I REBUILT and converted to CS operation. It now has over 3,600 TT, 430 TSOH (Rebuilt to NEW spec). I had the prop balance in December. Readings were .4 before and .1 after. The readings at 1,500 and 2,400 were out of phase when we started but everything was the same when it was done. The $100 for the prop balance is the best thing I ever did for the airplane. It is like a NEW airplane. The A&P that did the work use to do all the helicopters at the helo shop that was at the airport. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
Date: Jan 23, 2000
From: n3773 <n3773(at)mciworld.com>
Subject: Scott McD
I had wrongly assumed, that's why I'm not a CEO I guess, that Scott was helping us all while on the clock. He was responding from home, his own time. When everyone talks about low kit prices they should remember that there are employees and wages involved too. It's sad that a guy who clearly loves his job and volunteers his personal time to help us has to take a lot of grief too. I hope Van's can find the time to let him resume contributing to the RV-List from work should he want to. Kevin do not archive ________________________________________________________________________________
Date: Jan 24, 2000
From: n3773 <n3773(at)mciworld.com>
Subject: common radio freq.
That's why I'm hooked on this list, I'm always learning something new. Voice Comm. Frequencies, spelled out in the ol' AOPA, flight test stations of aircraft mfgs., 123.125 thru 123.575, except 123.30 & 123.50. Personally, I don't like tuning in the .025 in between channels. The catchy one, 123.45 has been discovered. So I just start at the beginning and choose 123.20? I suppose the "any RV's out there?" on 122.75 works just as well. I have noticed on two different trips to Seattle that pilots up there were using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" when conversing with the tower. I suppose that "Experimental" isn't very descriptive and covers a wider gamut than "Cessna" (remember they also say "twin Cessna"). Is this becoming common practice elsewhere? Kevin do not archive ________________________________________________________________________________
Date: Jan 24, 2000
From: Doug Gray <doug.gray(at)hlos.com.au>
Subject: Proseal measuring balance
Can someone tell me where I can find a picture of the 10:1 balance to weigh out the proseal? Doug Gray ________________________________________________________________________________
From: "Cy Galley" <cgalley(at)accessus.net>
Subject: Re: Prop Balancing
Date: Jan 24, 2000
I would check for a bad alternator belt. Cy Galley - Editor, B-C Contact! (Click here to visit our Club site at http://www.bellanca-championclub.com) -----Original Message----- From: Gary A. Sobek <rv6flier(at)yahoo.com> Date: Monday, January 24, 2000 2:45 AM Subject: Re: RV-List: Prop Balancing > >> >> some of you guys seem to know a bunch about >> balancing, so i'm gonna ask >> about my cherokee. its a 62' 160 hp conical mount >> lycoming. i had it >> balanced by a local and he couldn't do it cause the >> "numbers" kept changing. >> its swinging a sensinich that was sent out to be >> staticly balanced. i seem >> to have a pretty good vibe but my mechanic insists >> the old conical mounts >> (system not rubber) were the culprit. the motor was >> just overhauled 60 hrs >> ago by pen yann. >> >> any ideas???? >> capsteve(at)wzrd.com >> Steve DiNieri >> > >If there is something wrong with an accessory or other >rotating part of the engine, the prop balance will >give a reading like you are having. > >I have a CONICAL mount O-320 B2B that I REBUILT and >converted to CS operation. It now has over 3,600 TT, >430 TSOH (Rebuilt to NEW spec). I had the prop >balance in December. Readings were .4 before and .1 >after. The readings at 1,500 and 2,400 were out of >phase when we started but everything was the same when >it was done. > >The $100 for the prop balance is the best thing I ever >did for the airplane. It is like a NEW airplane. The >A&P that did the work use to do all the helicopters at >the helo shop that was at the airport. > > >==== >Gary A. Sobek >"My Sanity" RV-6 N157GS O-320 Hartzell, >Flying So. CA, USA >Talk to your friends online with Yahoo! Messenger. >http://im.yahoo.com > > ________________________________________________________________________________
From: "Dalski, Dave" <dave.dalski(at)eds.com>
Subject: Gas Cap Engraving
Date: Jan 24, 2000
Steve, I would like to get my caps engraved. I have them ready to ship today (Monday, 1/24. Am I too late, or should I ship them to you? Please advise. Dave Dalski 972-797-3350 -----Original Message----- From: PANELCUT(at)aol.com [mailto:PANELCUT(at)aol.com] Sent: Wednesday, January 19, 2000 8:42 AM Subject: Re: RV-List: Gas Cap Engraving Tom and Listers This is the last week for those that have not got there caps in. I will start them Monday. Sorry about the delay but would like to give a few people who have told me they sent their caps time to get here. For those who want to send them that haven't now is the time to do so. If they are a little late that's OK but prefer you send them NOW. Listed below are the one's I have received so far. I also have a few that were redo's from last time that will be done with this batch I hope this hasn't delayed anyone but I just decided to do all when I set them up. John Warren Bill Gibbs Robert Acker Craig Weiler Jim Wendel Kevin Belue David Plerson Tom Ervin Dale Wotring Pete Bodie Mel Jordan Gerald Forrest Randy Pflanzer Steven Cole Scott Chambers Curtis Shoemaker Thanks Steve Davis ________________________________________________________________________________
Date: Jan 24, 2000
From: "dgmurray" <dgmurray(at)telusplanet.net>
Subject: Re: Proseal measuring balance
Subject: RV-List: Proseal measuring balance > >Can someone tell me where I can find a picture of the 10:1 balance to >weigh out the proseal? > >Doug Gray Doug - I don't know which model you are building, or when you started, but there is a tips section in the back of my builders manual that has a picture of this balance you describe. It is also in the "14 Years of the RVator. Hope this helps, Doug Murray RV-6 Southern Alberta ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: SMALL NUTS
Jet nuts are another solution for a smaller nut that will still fit in a standart #3 or #4 bolt. There is a proper MS number for these nuts but are commonly called jet nuts. Sometimes you see them on exhaust bolts and obviously on jets. There are all metal and not all that pricey. I use 'em like cherry max rivets.......Got a bunch of 'em just in case and they do come in handy. ________________________________________________________________________________
From: "Tommy Walker" <twsurveyor(at)email.msn.com>
Subject: RV 6A F-670 Side Skin Rivits
Date: Jan 24, 2000
Plan sheet #36 shows 426 AD 4-6 rivits along the main longeron @ 1-1/2" spacing to attach the F-670 side skin. Question is how far back do you use the 4-6 rivits? I'm assuming (looking at the plans) they are used from the firewall back to the 605 bulkhead, then you use the 426 AD 3-5's from there back. Any advise is welcome! Tommy Ridgetop, TN ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Harmon Rocket Information
Guys, remember that Harmon Rocket IS NOT Team rocket. John Harmon can be reached via AOL & resides in California & the good folks at Team Rocket are in Texas & Florida.... Both Rocket companys offer a great toy but each have a different approach to the building process & design. Kinda close & kinda not. Both are great and it depends where the builder wants to position himself.. One is the HR-II and the other is the F-1... bobdz(at)email.msn.com on 01/21/2000 06:00:18 PM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: Harmon Rocket Information > > Does anyone have any information on a Harmon Rocket website or somewhere that I believe it is www.teamrocketaircraft.com ________________________________________________________________________________
Subject: Re: common radio freq.
Date: Jan 24, 2000
From: Larry Pardue <n5lp(at)carlsbad.net>
> > > I have noticed on two different trips to Seattle that pilots up >there were >using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" when >conversing with the tower. I suppose that "Experimental" isn't very >descriptive and covers a wider gamut than "Cessna" (remember they also say >"twin Cessna"). Is this becoming common practice elsewhere? Kevin do >not archive > > There is a legal requirement to identify yourself as experimental to ATC, at least in my operating limitations. My solution is to say experimental RV on initial call, then RV, but there are a lot of exceptions. I have been growled at for not identifying as an RV and have been growled at for doing it. My experience is that centers absolutely do not care. A lot of tower controllers, especially the sharper ones, do care. I was growled at at Lubbock the other day for saying RV and not specifying what kind. There are some sharp controllers, and incidently, RV builders there. At non-controlled fields RV or RV-x would seem to be always the proper procedure. Just my opinion. Larry Pardue Carlsbad, NM RV-6 N441LP http://www.carlsbadnm.com/n5lp/index.htm ________________________________________________________________________________
Date: Jan 24, 2000
From: George True <true(at)uswest.net>
Subject: Re: I sell Palm Pilots
Paul, Check out the moving map software at www.controlvision.com and tell me what you think. Can you also get the Casio or HP or Compac palmtop computers? I may be interested in getting a Palm Pilot from you. That AirCalc software is really neat. George Paul Besing wrote: > > I work for a computer distributor. If any of you would like a Palm Pilot, I > probably can get you one for what the resellers pay. Let me know off list > what your costs are, and we'll see what I can get them for. I would be > happy to pass these on at my cost to RV-Listers. > > Paul Besing > RV-6A (197AB) Arizona > http://members.home.net/rv8er > Finish Kit > ________________________________________________________________________________
Date: Jan 24, 2000
From: Denny Harjehausen <harje(at)proaxis.com>
Subject: Re: common radio freq.
>> I have noticed on two different trips to Seattle that pilots up >>there were >>using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" when >>conversing with the tower. I recall a blurb in one of the magazines a couple of years or so back that it was exceptable by the FAA to use "Glasair" or "Lancair" instead of "Experimental". Using "RV" some aurgue that it easy to confused with "Army", and the prefered was "Van's 641DH". If it was my choice it would be "RV641DH" on initial and "RV1DH" there after. But then I am very use to "RV". Have a great day! Denny, RV-6 N641DH (Flying) ________________________________________________________________________________
From: "Randy Lervold" <randyl(at)pacifier.com>
Subject: Re: common radio freq.
Date: Jan 24, 2000
> I have noticed on two different trips to Seattle that pilots up there were > using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" when > conversing with the tower. I suppose that "Experimental" isn't very > descriptive and covers a wider gamut than "Cessna" (remember they also say > "twin Cessna"). Is this becoming common practice elsewhere? Kevin do > not archive My understanding is that initiating your call to any ATC with "experimental 999XX" was the proper way to comply with the FARs which require, and I forget the language or the part, to make ATC aware that you are an experimental (as opposed to a certified) craft. Anyone know for sure? Das fed? Randy Lervold RV-8, #80500, panel & canopy skirt www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
From: DWENSING(at)aol.com
Date: Jan 24, 2000
Subject: Re: tube flaring w/ Rolo-flare tool
In a message dated 1/23/00 10:12:38 PM Central Standard Time, russnichols(at)msn.com writes: << the flare I produce isn't "centered". It gives me a nice surface in the tube, but one side of the tube doesn't flare out on the outside while the other has an extreme flare. >> Russ just another thought....check to see if both of the "gripping" wheels are indexed to the same size tubing. Sounds like the tubing and the cone are not concentric. Dale Ensing 6A Cary IL ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: Attn RV-4 builders/flyers: Advice sought
Date: Jan 24, 2000
I am building an RV-4 and am at the stage where the manual says that I'm supposed to start putting the skin on. Is there anything I should do now that would be easier to do prior to skinning? Things you would do different if you had it to do over again? Thanks in advance for your helpful advice! -- Scott VanArtsdalen, MCSE Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: EARL FORTNER [SMTP:e.fortner(at)worldnet.att.net] Sent: Saturday, January 22, 2000 1:07 AM To: rv-list(at)matronics.com Subject: Re: RV-List: RV4, F-482 That is the rear seat reinforcement. Call Vans and tell them you want the service bulletin and kit for the rear seat reinforcement. They will send you everything you need at no charge. Joe Wiza wrote: > > > Friend of mine bilding an RV4 can't find any info on PN F-482 left and > right. Does anyone know where they go or better print #. TU > > planejoe(at)ewol.com > ________________________________________________________________________________
Date: Jan 24, 2000
From: Bill VonDane <bvondane(at)atmel.com>
Subject: Capacitance Senders...
The other day I read a web page that had detailed instructions on building your own capacitance fuel sending units... Now I can't find it anywhere. Anyone know where I can find this again? Thanks... -Bill Von Dane - Colorado Springs, CO RV-8A N912V res., wing kit should be here by now! http://vondane.tripod.com ________________________________________________________________________________
Date: Jan 24, 2000
From: Larry Olson <lolson(at)doitnow.com>
Subject: Re: RV 6A F-670 Side Skin Rivits
I think you got it Tommy. Note: From the 605 back I used 3" spacing on the 3-5's for the bottom skin to the longeron, then 1" spacing on the top skin to the longeron. (the 1st hole already drilled from the bottom skins) Watch your spacing where the bulkheads line up. Make sense? If not, let me know. I'll clarify. Larry Olson Cave Creek, AZ RV6 - fitting canopy >I'm assuming (looking at the plans) they are used from the >firewall back to the 605 bulkhead, then you use the 426 AD 3-5's from there >back. Any advise is welcome! > >Tommy >Ridgetop, TN > ________________________________________________________________________________
From: donspawn(at)juno.com
Subject: RV 6A F-670 Side Skin Rivits
Date: Jan 24, 2000
Tom: Geroge O in the vedio suggested flush 3's on 3/4 inch spacing to do a better job of holding the skin down. Also, c/s the f601 before you nail the side down. I have to un-rivet some of mine. Well first mistake. Don Jordan ~ 6A fuselage ~ Arlington,Tx ~ donspawn(at)juno.com ****************************************************************************** writes: > > >Plan sheet #36 shows 426 AD 4-6 rivits along the main longeron @ >1-1/2" >spacing to attach the F-670 side skin. Question is how far back do you >use >the 4-6 rivits? I'm assuming (looking at the plans) they are used from >the >firewall back to the 605 bulkhead, then you use the 426 AD 3-5's from >there >back. Any advise is welcome! > >Tommy >Ridgetop, TN ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Attn RV-4 builders/flyers: Advice sought
One item that saved me some grief while installing the rear fuse skins....the bottoms (skins) are done first like you know. You clecko the longerron and invert the fuse. so now the fuse. is right side up and begin fitting the top skin...all's well so far. When you try to wrap the top skin down to the longerron the cleckos are in the way. You don't want to remove em' because any allignment or strength the fuse. has will be somewhat lost.......I ended up using the hand squeezer and riveting the bottom skin to the longerron then marking where the rivets were with a extended line, then installed the top skin with my ratchet straps. The top skin layed down nicely and I transfered my displaced lines and drilled & riveted the top skin on. Net result -twice as many rivets on the longeron but no harm or no foul anywhere. It only took about twenty minutes to hand squeeze the bottom skins on because the yoke fit over the longerron.......I also tilted the passanger seat bulkhead back (at the top) about two inches. The canopy still fits & there is more room to sneak in & out of the rear seat area. The seat also tilts back and is a whole lot more comfortable to be somewhat reclined. ....good luck. BTW the seat back-to-rear bulkhead reinforcements took 30 minutes to install - not a big thing..... svanarts(at)unionsafe.com on 01/24/2000 11:08:47 AM Please respond to rv-list(at)matronics.com Subject: RV-List: Attn RV-4 builders/flyers: Advice sought I am building an RV-4 and am at the stage where the manual says that I'm supposed to start putting the skin on. Is there anything I should do now that would be easier to do prior to skinning? Things you would do different if you had it to do over again? Thanks in advance for your helpful advice! -- Scott VanArtsdalen, MCSE Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: EARL FORTNER [SMTP:e.fortner(at)worldnet.att.net] Sent: Saturday, January 22, 2000 1:07 AM To: rv-list(at)matronics.com Subject: Re: RV-List: RV4, F-482 That is the rear seat reinforcement. Call Vans and tell them you want the service bulletin and kit for the rear seat reinforcement. They will send you everything you need at no charge. Joe Wiza wrote: > > > Friend of mine bilding an RV4 can't find any info on PN F-482 left and > right. Does anyone know where they go or better print #. TU > > planejoe(at)ewol.com > ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)mari.net>
Subject: Re: Capacitance Senders...
Date: Jan 24, 2000
Bill: Look in the Bunny Guide under Building the tanks. I believe there is an article there written by Dick Martin, who is responsible for the development of the Capacitance senders that Vans sells. Hope this helps Regards, Jeff Orear RV6A 25171 second wing---skeleton Peshtigo, WI -----Original Message----- From: Bill VonDane <bvondane(at)atmel.com> Date: Monday, January 24, 2000 11:30 AM Subject: RV-List: Capacitance Senders... > >The other day I read a web page that had detailed instructions on building >your own capacitance fuel sending units... Now I can't find it anywhere. >Anyone know where I can find this again? > >Thanks... > >-Bill Von Dane - Colorado Springs, CO >RV-8A N912V res., wing kit should be here by now! >http://vondane.tripod.com > > ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)mari.net>
Subject: Flairing tool advice
Date: Jan 24, 2000
Hi: One other thing that I have not seen mentioned is to make sure that you do not have the tubing sticking up too far above the flaring tool. My first attempt at tube flaring resulted in the kind of flair that you are describing as a result. Regards, Jeff Orear RV6A 25171 Second wing---skeleton Peshtigo, WI ________________________________________________________________________________
From: CW9371(at)aol.com
Date: Jan 24, 2000
Subject: Re: Harmon Rocket Information
In a message dated 1/24/2000 9:04:16 AM Central Standard Time, pcondon(at)csc.com writes: << Guys, remember that Harmon Rocket IS NOT Team rocket. John Harmon can be reached via AOL & resides in California & the good folks at Team Rocket are in Texas & Florida.... Both Rocket companys offer a great toy but each have a different approach to the building process & design. Kinda close & kinda not. Both are great and it depends where the builder wants to position himself.. One is the HR-II and the other is the F-1... >> Dont forget that mark of Team Rocket can help you out with stuff for your RV's and Harmon rockets as thats what he was building for people before he and Scott formed Team Rocket. They have some great fairings for all 3 aircraft and they also have a slider canopy for the Harmon Rocket. But you do have a good point they are seperate companies. Chris Wilcox F-1 Rocket Builder ________________________________________________________________________________
Date: Jan 25, 2000
From: Frank and Dorothy <frankvdh(at)ihug.co.nz>
Subject: Re: Proseal measuring balance
Doug Gray wrote: > > > Can someone tell me where I can find a picture of the 10:1 balance to > weigh out the proseal? http://members.xoom.com/frankv/bunny2c.htm has some instructions, plus a link to a photo. Frank. ________________________________________________________________________________
From: "Michael Robertson" <mrobert569(at)hotmail.com>
Subject: Re: common radio freq.
Date: Jan 24, 2000
Talk about opening a can of worms here. Before I get into this I will admit that there have been memos and letters wandering aroung the system that I am fully unaware of and each region within the US may have slight alterations to their specific regions. In writing that we all have access to there are two examples. FAR 91.319(d(3) says that we have to advise "tower" of the experimental nature of our aircraft when operating out of a field with an operating control tower. To get to a bit more/better information we need to look at the Airman's Information Manual (AIM) in paragraph 4-2-4 which covers aircraft call signs. It says they we are supposed to fully identify our aircraft on the intial call. ATC may then abbreviate the callsign. After that we may use the abbreviatied format. It then goes on to state that "civil" aircraft pilots should state the aircraft type, the manufacturer's name or model, followed by the registration number. For example: "Tower, this is Experimental Van's (or RV8) 108RS". The "N" is not needed unless the aircraft is of foreign registry. So if you fly to Canada or Mexico remember to add it on first contact. Mike Robertson RV-8A QB "Das Fed" >From: "Randy Lervold" <randyl(at)pacifier.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: Re: RV-List: common radio freq. >Date: Mon, 24 Jan 2000 08:01:09 -0800 > > > > I have noticed on two different trips to Seattle that pilots up >there were > > using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" >when > > conversing with the tower. I suppose that "Experimental" isn't very > > descriptive and covers a wider gamut than "Cessna" (remember they also >say > > "twin Cessna"). Is this becoming common practice elsewhere? Kevin >do > > not archive > > >My understanding is that initiating your call to any ATC with "experimental >999XX" was the proper way to comply with the FARs which require, and I >forget the language or the part, to make ATC aware that you are an >experimental (as opposed to a certified) craft. > >Anyone know for sure? Das fed? > >Randy Lervold >RV-8, #80500, panel & canopy skirt >www.pacifier.com/~randyl >Home Wing VAF > > ________________________________________________________________________________
Date: Jan 25, 2000
From: Frank and Dorothy <frankvdh(at)ihug.co.nz>
Subject: Re: Capacitance Senders...
Bill VonDane wrote: > > > The other day I read a web page that had detailed instructions on building > your own capacitance fuel sending units... Now I can't find it anywhere. > Anyone know where I can find this again? http://members.xoom.com/frankv/bunny2c.htm has my experiences, plus information provided by (IIRC) Dick Martin on how he did them. Frank. ________________________________________________________________________________
From: "Van Artsdalen, Scott" <svanarts(at)unionsafe.com>
Subject: common radio freq.
Date: Jan 24, 2000
I will probably make the initial call something like, "Podunk tower, experimental 311SV, an RV-4, inbound with whiskey." (or gin, or vodka). After that I will shorten it to just "RV 1SV." -- Scott VanArtsdalen, MCSE Network Administrator Union Safe Deposit Bank 209-946-5116 -----Original Message----- From: Randy Lervold [SMTP:randyl(at)pacifier.com] Sent: Monday, January 24, 2000 8:01 AM To: rv-list(at)matronics.com Subject: Re: RV-List: common radio freq. > I have noticed on two different trips to Seattle that pilots up there were > using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" when > conversing with the tower. I suppose that "Experimental" isn't very > descriptive and covers a wider gamut than "Cessna" (remember they also say > "twin Cessna"). Is this becoming common practice elsewhere? Kevin do > not archive My understanding is that initiating your call to any ATC with "experimental 999XX" was the proper way to comply with the FARs which require, and I forget the language or the part, to make ATC aware that you are an experimental (as opposed to a certified) craft. Anyone know for sure? Das fed? Randy Lervold RV-8, #80500, panel & canopy skirt www.pacifier.com/~randyl Home Wing VAF ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Prop Balancing
I think your mechanic is talking thru his hat. If indeed the rubbers are shot you could tell by the sag...at any rate the rubbers are very cheap (wag aero among others) for the conical motor. Check your alt/gen mount(s) for broken or misalligned mounts and tentioning arm, check torque on prop and be sure the drive lugs are snug and that the prop tracks (blade track). A dial guage will show out-o-round on the crank flange, try another prop shop with a technical who knows what he is doing..........ALSO, when finished mark tthe prop to the crank flange in case its yanked later & count all washers and index the spinner plates so the WHOLE rotating mass can be reassembled and the ballance kept... rv6flier(at)yahoo.com on 01/24/2000 02:50:35 AM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: Prop Balancing > > some of you guys seem to know a bunch about > balancing, so i'm gonna ask > about my cherokee. its a 62' 160 hp conical mount > lycoming. i had it > balanced by a local and he couldn't do it cause the > "numbers" kept changing. > its swinging a sensinich that was sent out to be > staticly balanced. i seem > to have a pretty good vibe but my mechanic insists > the old conical mounts > (system not rubber) were the culprit. the motor was > just overhauled 60 hrs > ago by pen yann. > > any ideas???? > capsteve(at)wzrd.com > Steve DiNieri > If there is something wrong with an accessory or other rotating part of the engine, the prop balance will give a reading like you are having. I have a CONICAL mount O-320 B2B that I REBUILT and converted to CS operation. It now has over 3,600 TT, 430 TSOH (Rebuilt to NEW spec). I had the prop balance in December. Readings were .4 before and .1 after. The readings at 1,500 and 2,400 were out of phase when we started but everything was the same when it was done. The $100 for the prop balance is the best thing I ever did for the airplane. It is like a NEW airplane. The A&P that did the work use to do all the helicopters at the helo shop that was at the airport. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: common radio freq.
I , like most folks registered my last name in the aircraft type line of the application and the official document from FAA says nothing about Vans......this could lead to some more confusion if some builders used their last names in the identification of their aircraft. Whats wrong announcing experimental RV on the radio? I for one look exrta hard when I hear the word experimental because I know most experimentals now a days are fast and small and harder to see.......Any others think along these lines ?? mrobert569(at)hotmail.com on 01/24/2000 01:21:36 PM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: common radio freq. Talk about opening a can of worms here. Before I get into this I will admit that there have been memos and letters wandering aroung the system that I am fully unaware of and each region within the US may have slight alterations to their specific regions. In writing that we all have access to there are two examples. FAR 91.319(d(3) says that we have to advise "tower" of the experimental nature of our aircraft when operating out of a field with an operating control tower. To get to a bit more/better information we need to look at the Airman's Information Manual (AIM) in paragraph 4-2-4 which covers aircraft call signs. It says they we are supposed to fully identify our aircraft on the intial call. ATC may then abbreviate the callsign. After that we may use the abbreviatied format. It then goes on to state that "civil" aircraft pilots should state the aircraft type, the manufacturer's name or model, followed by the registration number. For example: "Tower, this is Experimental Van's (or RV8) 108RS". The "N" is not needed unless the aircraft is of foreign registry. So if you fly to Canada or Mexico remember to add it on first contact. Mike Robertson RV-8A QB "Das Fed" >From: "Randy Lervold" <randyl(at)pacifier.com> >Reply-To: rv-list(at)matronics.com >To: >Subject: Re: RV-List: common radio freq. >Date: Mon, 24 Jan 2000 08:01:09 -0800 > > > > I have noticed on two different trips to Seattle that pilots up >there were > > using "Glasair" and "Lancair" and yes, "RV" rather than "Experimental" >when > > conversing with the tower. I suppose that "Experimental" isn't very > > descriptive and covers a wider gamut than "Cessna" (remember they also >say > > "twin Cessna"). Is this becoming common practice elsewhere? Kevin >do > > not archive > > >My understanding is that initiating your call to any ATC with "experimental >999XX" was the proper way to comply with the FARs which require, and I >forget the language or the part, to make ATC aware that you are an >experimental (as opposed to a certified) craft. > >Anyone know for sure? Das fed? > >Randy Lervold >RV-8, #80500, panel & canopy skirt >www.pacifier.com/~randyl >Home Wing VAF > > ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Breaker/switch orientation
If you are going to use breakers then the bus bar used to connect the breakers does influence the way you mount the breakers i.e. in a straight line....... ________________________________________________________________________________
Date: Jan 24, 2000
From: "Gary A. Sobek" <rv6flier(at)yahoo.com>
Subject: Initial Radio Call
My procedure may not be correct or the best but I have been using it for the last 1.5 years. I start my first radio call as: (Tower, ATC facility, or Airport name)"EXPERMENTAL RV 1 5 7 Gulf Sierra" position, altitude, and (request / intention). After the initial call, I respond "RV 7 Gulf Sierra". Most (40%) of the SoCAL controllers respond NOVEMBER 7 Gulf Sierra, but (30%) EXPERMENTAL and (30%) RV are used by the rest. If asked for type, I use to respond RV-6/Gulf. I now respond Romeo Victor Six / Gulf as one controller listed me in the system as an RB-6. The next controller questioned me on that. /Gulf my not be correct as I do not have GPS approach capabilities. (According to 1999 FAR / AIM 5-1-7 TBL 5-1-2) I try to abide by the FARs as best I can. I feel that I am doing that by my understanding of them. I am sure that not everyone will agree. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: "Bryan E. Files" <bfiles(at)corecom.net>
Subject: Prop Balancing
Date: Jan 24, 2000
I have also seen a lot of the rubber mounts installed wrong. There is a compression one that goes opposite on top than on bottom. ***Bryan E. Files*** A&P, IA, FAA Safety Counselor Fat City Aircraft Palmer, Alaska mailto:BFiles(at)corecom.net -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of pcondon(at)csc.com Sent: Monday, January 24, 2000 9:55 AM Subject: Re: RV-List: Prop Balancing I think your mechanic is talking thru his hat. If indeed the rubbers are shot you could tell by the sag...at any rate the rubbers are very cheap (wag aero among others) for the conical motor. Check your alt/gen mount(s) for broken or misalligned mounts and tentioning arm, check torque on prop and be sure the drive lugs are snug and that the prop tracks (blade track). A dial guage will show out-o-round on the crank flange, try another prop shop with a technical who knows what he is doing..........ALSO, when finished mark tthe prop to the crank flange in case its yanked later & count all washers and index the spinner plates so the WHOLE rotating mass can be reassembled and the ballance kept... rv6flier(at)yahoo.com on 01/24/2000 02:50:35 AM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: Prop Balancing > > some of you guys seem to know a bunch about > balancing, so i'm gonna ask > about my cherokee. its a 62' 160 hp conical mount > lycoming. i had it > balanced by a local and he couldn't do it cause the > "numbers" kept changing. > its swinging a sensinich that was sent out to be > staticly balanced. i seem > to have a pretty good vibe but my mechanic insists > the old conical mounts > (system not rubber) were the culprit. the motor was > just overhauled 60 hrs > ago by pen yann. > > any ideas???? > capsteve(at)wzrd.com > Steve DiNieri > If there is something wrong with an accessory or other rotating part of the engine, the prop balance will give a reading like you are having. I have a CONICAL mount O-320 B2B that I REBUILT and converted to CS operation. It now has over 3,600 TT, 430 TSOH (Rebuilt to NEW spec). I had the prop balance in December. Readings were .4 before and .1 after. The readings at 1,500 and 2,400 were out of phase when we started but everything was the same when it was done. The $100 for the prop balance is the best thing I ever did for the airplane. It is like a NEW airplane. The A&P that did the work use to do all the helicopters at the helo shop that was at the airport. ==== Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, Flying So. CA, USA Talk to your friends online with Yahoo! Messenger. http://im.yahoo.com ________________________________________________________________________________
From: "lucky macy" <luckymacy(at)hotmail.com>
Subject: Wing Levelors compatible with Quick Build kits?
Date: Jan 24, 2000
Anyone know of any wing levelors that are compatible with the quick build kits? TIA, lucky ________________________________________________________________________________
From: "Linzel G . Civ - 43CES/CECP" <Gray.Linzel(at)pope.af.mil>
Subject: RV3 Performance Enhancements
Date: Jan 24, 2000
Has anyone made any minor airframe modifications to a stock RV3 like additional fairings, gap seals, etc. (unless they are keeping them secret) and noticed performance improvements. My RV3 flies as advertised which is great. However, I see nifty wing root fairings on some planes and Mooneys have nice tight aileron and elevator seals. If anyone has tried a mod and found it of questionable benefit or that it came with some undesirable side effect I'll know not to try it. Gray ________________________________________________________________________________
Date: Jan 24, 2000
From: Keith Hughes <rv6tc(at)earthlink.net>
Subject: Re: common radio freq.
I think the intent is to have you identify the type of aircraft for visual acquisition / identification purposes, for both the tower as well as other aircraft. If there were just two aircraft airborne in any given sector it wouldn't matter, but to help identify issued traffic, it helps determine the visual "shadow" of the aircraft. In fact, there was an accident in San Diego (I think it was early 80's), when a PSA (I think, could have been Western) B-727 misidentified traffic that was issued by SoCal Approach. The Aircraft struck a Cessna that was not acquired. Just saying "Experimental" doesn't necessarily accomplish the goal, because it could be an RV, a Glass star, or Kitfox, or a Velocity. I think you would agree that they all will look quite different. Despite who built the plane, the "Planform" is an RV-6, RV-8, etc. That's the way that I see it. Keith Hughes RV-6 Wings Parker, CO pcondon(at)csc.com wrote: > Whats wrong announcing > experimental RV on the radio? I for one look exrta hard when I hear the word > experimental because I know most experimentals now a days are fast and small > and harder to see.......Any others think along these lines ?? ________________________________________________________________________________
From: Jim_Andrews(at)tivoli.com
Date: Jan 24, 2000
Subject: Source for fuse blocks that take auto fuses
Anyone know of a good place to pick up a fuse block that will take auto fuses ( the knife variety ). I have decided to forgo the circuit breaker idea and just put in auto fuses. Thanks, - Jim Andrews RV-8A QB ( wings ) N89JA ( reserved ) ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Prop Balancing/Hinge Breakage
Relative to this thread....... is there any data to support more or less hinge damage on the rv-4 vs. the rv6 ?? The only reason I suggest this is the RV-4 cowl has tighter radius and less expance and hence less movement then the rv-6 ( theory at this point). For the same fiberglass thickness my rv-4 cowl seems to behave differently than my hanger mates' rv-6 cowl in terms of vibration & hinge breakage....Any real world testimonials?? alexpeterson(at)usjet.net on 01/22/2000 08:22:37 PM Please respond to rv-list(at)matronics.com Subject: Re: RV-List: Prop Balancing > > Any further breakage, at least I will know it is not vibration. > > Larry Pardue > Carlsbad, NM > > RV-6 N441LP Further breakage is likely to be caused by vibration, but not due to imbalances in the engine. The whole cowl can be thought of as a large collection of springs, each with its own natural frequency. If one could magically "see" inside the cowl when in flight, it might be surprising (or scary). I don't know specifically where your cowl hinges are breaking, but is it possible to fashion small brackets with rubber feet, which, when mounted to the firewall, apply some pressure outward on the cowl right near the hinge? Somehow, the natural frequency of the cowl in the area of breaking hinges needs to be changed, as it might be the same frequency as the prop pulses. Maybe glassing stiffener ribs in the cowl in the region of interest would also help. Just thoughts on what might help, not claiming they will work! Alex Peterson ________________________________________________________________________________
From: pcondon(at)csc.com
Date: Jan 24, 2000
Subject: Re: Engine Baffles/Cowl removal Aid
The only recommendation that I have regarding fitting baffles to the engine, is to make a cardboard template where the baffle goes against the engine and then use the template as a guide to cut the baffle. IMHO, this will save time in the long run. The cardboard ( folders from work - donated with out consent) trick worked for me too. I used the folders taped to my bafffles and cut the folder material with scissors. Worked great. When completed, I cut my metal baffles once. For the cowl removal aid I made a craddle made up from two sissors jacks bolted onto a metal milk crate which I bolted to a mechanics creeper. The two scissor jacks have a short run of 1 x 6 pine with pipe insulation installed on top.......I roll the "science fair project" up to the RV, tweek the two sissor jacks up to catch the botttom cowl, pull my pins & then tweek the sissor jacks down with my fingers.....when clear of everything I roll the craddle away. Works great & the three other RV builders at my airport have just about wore the wheels off my craddle rolling it from their hangers to my hanger. This makes the hundred or so cowl fitting attempts and regular maintenance a one man affair. Cost- about 5 dollars & a well stocked junk filled garage. The jacks were from Subaru's but the only thing that matters is the jacks be small and of the same geometery and thread pitch. ________________________________________________________________________________
Date: Jan 24, 2000
From: Michael Hartmann <hartmann(at)sound.net>
Subject: Re: common radio freq.
>There is a legal requirement to identify yourself as experimental to ATC, >at least in my operating limitations. My solution is to say experimental >RV on initial call, then RV, but there are a lot of exceptions. > >I have been growled at for not identifying as an RV and have been growled >at for doing it. My experience is that centers absolutely do not care. >A lot of tower controllers, especially the sharper ones, do care. I was >growled at at Lubbock the other day for saying RV and not specifying what >kind. There are some sharp controllers, and incidently, RV builders If the requirement is specified in the operating limitations for your aircraft, then comply. If not, there is a requirement to identify the experimental nature of the aircraft to TOWER on INITIAL contact. Beyond that, call it whatever you like. I prefer "November", but "RV", or "experimental", is just fine. If calling center (ARTCC), we couldn't care less about the type, except those of us who are into airplanes. I enjoy calling the overtaking traffic to the malibu, mooney, and bonanza drivers. Yeah, just another $35000 homebuilt. So move over and get out of it's way. If I got "growled" at by any controller for not being specific with the type, I'd growl right back. Anyone familiar with the series knows there's no significant difference in size, weight, or performance between the types. Especially from a controller's perspective. - Mike (Full time controller for more than half my life...and still loving it) ________________________________________________________________________________
From: "Brian Denk" <akroguy(at)hotmail.com>
Subject: Re: Source for fuse blocks that take auto fuses
Date: Jan 24, 2000
> >Anyone know of a good place to pick up a fuse block that will take auto >fuses ( >the knife variety ). > >I have decided to forgo the circuit breaker idea and just put in auto >fuses. > >Thanks, > >- Jim Andrews >RV-8A QB ( wings ) >N89JA ( reserved ) Jim, Good choice on using the fuse blocks. I put in two of them, each has slots for up to ten circuits, and they use standard automotive blade fuses. I found them at a local automotive electrical supply store for about $10 each. They are very lightweight and I mounted them to the aft side of the front baggage hold bulkhead. I cut an access hole in the bulkhead as a few other RV8 builders have also done to access the blocks and the rear of the instruments. A simple piece of alclad sheet is used as a cover and held in place via nutplates. I think the fuse blocks are made by Cole Hersey. So, you might call a local auto parts supply store and just ask if they carry electrical parts from this company. They also make all kinds of solenoids for use as master and starter contactors. Brian Denk RV8 N94BD fast-ons, fuseblocks and flying. ________________________________________________________________________________
Date: Jan 24, 2000
From: Richard Reynolds <RVReynolds(at)macs.net>
Subject: Re: Source for fuse blocks that take auto fuses
Jim_Andrews(at)tivoli.com wrote: "..know of a good place to pick up a fuse block that will take auto fuses.." Try "Electric Bob's AeroElectric Connection <http://www.aeroelectric.com/. Also West Marine and BoatsUS have the 4 and 6 fuse blocks. Bob has those plus 10 and 20 fuse blocks and lots of other stuff. Richard Reynolds, Norfolk, VA, RV-6A, doing the panel while its cold. ________________________________________________________________________________
Date: Jan 24, 2000
From: "Owens" <owens(at)aerovironment.com>
Subject: Source for fuse blocks that take auto fuses
Jim, Try the aeroelectric connection at: http://www.aeroelectric.com/Catalog/catalog.html Lots of goodies you'll need. Laird RV-6 22923 (with fuses) SoCal Anyone know of a good place to pick up a fuse block that will take auto fuses ( the knife variety ). I have decided to forgo the circuit breaker idea and just put in auto fuses. Thanks, - Jim Andrews ________________________________________________________________________________
Date: Jan 24, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Source for fuse blocks that take auto fuses
>>I have decided to forgo the circuit breaker idea and just put in auto >>fuses. > >I think the fuse blocks are made by Cole Hersey. So, you might call a local >auto parts supply store and just ask if they carry electrical parts from >this company. They also make all kinds of solenoids for use as master and >starter contactors. They are also offered in our website catalog at http://www.aeroelectric.com/Catalog/catalog.html Click on any item on the front page to link to the description and illustrations. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
From: "Bill Noel" <bnoel(at)ausa.net>
Subject: Re: Prop Balancing
Date: Jan 24, 2000
Remember that some of these chadwicks are old, susceptable to problems. As a rule, the stronger the vibe the easier to get "good numbers". On old balancers, the reflector would not be steady when you got below .1 ips or so. My 71 Cherokee I rebuilt felt good. I put the chadwick on and it was .8 ips! (real bad). @ adjustments and it went to .06. It's amazing how much quieter it got! If your mounts are not bad the reason sure isn't the design. The newer vibration equipment is very accurate and the tech can say not necessary cause you are .03 ( or whatever ) not that mounts design prevents balance. -----Original Message----- From: capsteve(at)wzrd.com <capsteve(at)wzrd.com> Date: Sunday, January 23, 2000 10:59 PM Subject: Re: RV-List: Prop Balancing > >some of you guys seem to know a bunch about balancing, so i'm gonna ask >about my cherokee. its a 62' 160 hp conical mount lycoming. i had it >balanced by a local and he couldn't do it cause the "numbers" kept changing. >its swinging a sensinich that was sent out to be staticly balanced. i seem >to have a pretty good vibe but my mechanic insists the old conical mounts >(system not rubber) were the culprit. the motor was just overhauled 60 hrs >ago by pen yann. > >any ideas???? >capsteve(at)wzrd.com >Steve DiNieri > > ________________________________________________________________________________
From: Lenleg(at)aol.com
Date: Jan 24, 2000
Subject: Re: Kevin Horton Updates
Kevin: Thank you so much for taking the time to continually give updates on your construction. I trail you in your progress by mere days (putting 8A fuselage in the jig) and have used your comments to help in my construction. I love this list !!! Len RV-8A Putting fuselage in jig ________________________________________________________________________________
Date: Jan 24, 2000
From: "John B. Abell" <jbabell(at)mediaone.net>
Subject: Re: common radio freq.
For several months, I've been under the impression that the proper language for contacting ATC would be, for example, "Los Angeles Center, RV6 12345 with you eight thousand level." However, when contacting a control tower, one is required to add "experimental," for example, "Santa Monica Tower, RV6 12345 experimental, inbound at the Palisades with information delta." The "RV6" type designation applies to both the RV-6 and the RV-6A. The experimental designation needs to be spoken only once, on initial contact with the control tower. No manufacturer's name is required. > My understanding is that initiating your call to any ATC with "experimental > 999XX" was the proper way to comply with the FARs which require, and I > forget the language or the part, to make ATC aware that you are an > experimental (as opposed to a certified) craft. > > Anyone know for sure? Das fed? > > Randy Lervold > RV-8, #80500, panel & canopy skirt > www.pacifier.com/~randyl > Home Wing VAF > ________________________________________________________________________________
From: "Robert Burns" <hsierra(at)flash.net>
Subject: Re: Capacitance Senders...
Date: Jan 24, 2000
jim weir has it on his page WWW.RST-ENGR.COM Robert Burns RV-4 s/n 3521 N82RB --> >The other day I read a web page that had detailed instructions on building >your own capacitance fuel sending units... Now I can't find it anywhere. >Anyone know where I can find this again? > >Thanks... > ________________________________________________________________________________
Date: Jan 24, 2000
From: Charlie and Tupper England <cengland(at)netdoor.com>
Subject: Re: common radio freq.
Michael Robertson wrote: > > > Talk about opening a can of worms here. Before I get into this I will admit > that there have been memos and letters wandering aroung the system that I am > fully unaware of and each region within the US may have slight alterations > to their specific regions. > In writing that we all have access to there are two examples. FAR > 91.319(d(3) says that we have to advise "tower" of the experimental nature > of our aircraft when operating out of a field with an operating control > tower. To get to a bit more/better information we need to look at the snips Mike, & other feds, In this area (Southeast), on 1st call to Approach or Tower the controller will ask for 'class' of experimental. The class tells the controller the cruise speed range of the a/c, with rv's being class B. Controllers are not very consistent with this, but a friend who's a controller has told me it's 'official.' Is this not a national practice? Charlie flying -4 ________________________________________________________________________________
From: Gusndale(at)aol.com
Date: Jan 24, 2000
Subject: Re: GPS and Map Compatibility
Listers, I need some advice about matching a IImorrow (UPS Aviation Technologies) SL-60 GPS/Com with a Skyforce Tracker moving map. I like the features of the SL-60 GPS/Com, especially nominating com frequencies on your route, but the Apollo 360 Map display from IImorrow is primitive compared to the detail available with the Skyforce Tracker moving map. Skyforce promotional material says that the Tracker maps are designed to interface with existing Loran and GPS receivers. I need to finalize my panel now. Anyone know if this will work well or if it will be a mistake because the two units won't speak the same language well enough to cooperate with each other? I'm ignorant of whether their are industry standards which make this as simple and viable as using a brand A stereo receiver with brand B speakers or not. I don't want to tackle making this work if it won't be a nice setup in the end. I'm pretty good at following directions and hooking wires up but I don't understand much about how these things work. I really hope this can work. Is this a doable idea that will work properly or an experiment that will likely not work very well? All responses appreciated. Thanks, Dale Wotring RV-6A working on panel (and still don't have a final equipment list) Vancouver, WA ________________________________________________________________________________
Date: Jan 24, 2000
Subject: Re: GPS and Map Compatibility
From: "Shelby Smith" <shelbyrv6a(at)mindspring.com>
I think the tracker is a little bulky(heard good things about it though) and there have been several post on combining GPSs with Palm Pilots and CE machines. This is the scenario I want to pursue. I like the beautiful CE displays. The handhelds have custom display software - so you know they will be upgrading and adding neat features. The Palm units have potential too. I like the UPS SL-60 too. I have been flying with a Lowrance 100 - the less expensive unit - it is fantastic! My .02 worth. -- Shelby Smith shelbyrv6a(at)mindspring.com RV6A - Skinning Fuselage - 200HP N95EB - reserved ---------- >From: Gusndale(at)aol.com >To: rv-list(at)matronics.com >Subject: Re: RV-List: GPS and Map Compatibility >Date: Mon, Jan 24, 2000, 9:12 PM > > I need some advice about matching a IImorrow (UPS Aviation Technologies) > SL-60 GPS/Com with a Skyforce Tracker moving map. I like the features of > the SL-60 GPS/Com, especially nominating com frequencies on your route, but > the Apollo 360 Map display from IImorrow is primitive compared to the detail > available with the Skyforce Tracker moving map. Skyforce promotional > material says that the Tracker maps are designed to interface with existing > Loran and GPS receivers. ________________________________________________________________________________
Date: Jan 24, 2000
From: "Robert L. Nuckolls, III" <nuckolls(at)aeroelectric.com>
Subject: Re: Electroair ignition
> >Bob, > >Whats the status of Revision-9? When do you think they might be ready to ship? Any price >changes? Looking to get it to printers in about two weeks. Should have some books by mid Feb. Bob . . . http://www.aeroelectric.com ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)petroblend.com>
Subject: Garmin e-map
Date: Jan 24, 2000
I went to the MSP boat show Sunday. The boat gadget peddlers were selling Garmin's latest and greatest, the "e-map". It is a little smaller than a palm pilot with a big screen and has 2 AA batteries and is supposed to last 22 hrs on them. It has some internal memory, looks like alot, plus an 8 to 16 mb removable cartridge. Has anyone seen an aviation version or aviation cartridge? Considering the Lowrance Airmap 100 only has 1 mb onboard, imagine what we can do with 16 meg!!!!!!! It truly will be a pocket sectional for the entire US!!!!!!!! They were selling these for $199 at the boat show plus $40 for a blank 8 mb cartridge this removable cartridge should allow for 3rd party vendors to sell aviation software at some bargain prices too!!!!!!!!! Man I love capitalism!!!!! Tailwinds Doug Rozendaal www.petroblend.com/dougr dougr(at)petroblend.com ________________________________________________________________________________
From: GlfrDug(at)aol.com
Date: Jan 24, 2000
Subject: Orlando RV'ers
I will be in Orlando for the big golf show from Mon Jan 31st evening until Tuesday am Feb.8th.....I will have a rental car and am willing to drive to see any projects in the Orlando area or out a ways.. I have an 8QB underway so seeing any other in progress 8's or even one flying would be great. Would love to catch a ride in a 6 or 4 if anyone would let me buy the gas as well. Thanks in advance....all that golf for 8 days is too much and it has been a little too cold to fly here in Northern Mich. Doug Bell 231-398-9106 Home 231-723-8874 Work 8QB, Wings done, back to the fuse, waiting for finish kit ________________________________________________________________________________
From: Arzflyer(at)aol.com
Date: Jan 24, 2000
Subject: re:subscribe
arzflyer(at)aol.com subscribe ________________________________________________________________________________
From: RClayp5888(at)aol.com
Date: Jan 25, 2000
Subject: Re: Wing Levelors compatible with Quick Build kits?
I installed the Navaid under the right seat. Have not flown yet, but was easy to install and think it will work fine. Bob Claypool 428BC (reserved) almost there in the sky ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: GPS and Map Compatibility
Date: Jan 25, 2000
Dale, We liked the SL-60 and looked at the 360, but ultimately decided to go with the SL-40 and mount a Garmin 195 on a mount below our horizon. We made this decision based on the fact that we expect many changes to take place in the next year or two (from a tachnology & cost perspective). The result of this decision is that we can use the "195" as a moving map as well as an HSI, in a VFR config. Within a couple a years we'll have the "195" as a backup GPS to what ever we install as a full IFR capable GPS and install an electric DG. These are difficult decisions but it bacame easier when we decided to plan on the basis of where we wanted to be 2-3 years from now, while having a flying VFR RV-8A soon. Good Building, Chuck & Dave Rowbotham RV-8A Niantic, CT >From: Gusndale(at)aol.com >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: Re: RV-List: GPS and Map Compatibility >Date: Mon, 24 Jan 2000 22:12:44 EST > > >Listers, >


January 19, 2000 - January 25, 2000

RV-Archive.digest.vol-hu