RV-Archive.digest.vol-qu

April 24, 2005 - May 04, 2005



      
      
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From: Paul Folbrecht <paul.folbrecht(at)veribox.net>
Subject: QB Questions
Date: Apr 24, 2005
A couple general questions about QB kits. 1) Are there ever problems with getting enough access in the wings for installing autopilot servos, lights, or anything else? I know they come sans one skin only.. is that enough? 2) Any thoughts about the wash primer used? I know some ppl paint the inside of the fuse in addition to that. Why? The wash primer is deemed not sufficient for corrosion protection? ________________________________________________________________________________
Date: Apr 24, 2005
From: Scott VanArtsdalen <svanarts(at)yahoo.com>
Subject: Re: RV-List:
There is a product out there called Vikuiti which is made by 3m. If you ask they will send you a sample anti-glare screen filter. These REALLY work well. Charles Heathco wrote: > >I tried the 2000 out in the sum and it is unreadable on highest setting even. My 296 is readable in direct sunlight, but everything in the cockpit reflects off the screen which is anoying and makes it harder to see than if sun is directly on it. And of course, shortly after I bought it the price went down $200. Charlie heathco > > > > ________________________________________________________________________________
From: "Dale Ensing" <densing(at)carolina.rr.com>
Subject: Re: Aft Skirts
Date: Apr 24, 2005
Pete Howell Fitting the aft skirts on a slider....What worked for me on a 6 slider........ 1. Second person, leather gloves on, grips the lower edge of skirt with slider in forward closed position. 2. Pull hard forward and down and twist while you drill and cleco. Takes a lot of pull and twist to get a good fit so don't be timid. Dale Ensing ________________________________________________________________________________
From: "John Danielson" <Jdaniel343(at)bresnan.net>
Subject: Aft Skirts
Date: Apr 24, 2005
I used a shrinker to pull down the aft edges, after getting them as close possible by pulling them by hand. By using the shrinker, I got a a really tight fit. John L. Danielson -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Pete Howell Subject: RV-List: Aft Skirts <pete.howell@gecko-group.com> Hello, Anybody have any neat tricks to get the proper curve in the aft slider skirts? I have the tops nailed, but the twist along the bottom part is vexing. Cheers, Pete Howell ________________________________________________________________________________
Date: Apr 24, 2005
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Emergency notification (Was: RV-6 Crash)
Several days ago I flew around SE Utah (Monumwent Valley, Page AZ and Canyonlands/Moab UT) with another RV and one thing that the astute pilot will note is that there are few landing areas. If something looks smooth from 15500' it most likely is not. There were times when the other plane was not visible and exact location was unknown. So neither could have provided pinpoint directions to SAR personnel. When I travel alone I always use Flight following. Never bother with flight plans since constant contact with ATC provides immediate action if a problem develops. On the flight a few days ago, we were on 122.75 and no ATC. Never again. In addition, I am probably going to get a 406 PLB. If you are not aware, satellite coverage of 121.5 MHz will end in 2009 I believe, transitioning to 406 MHz which is supported now by a few GEO satellites and some LEO satellites as well. The advantage of 406 MHz is that it can include info about the owner (unique beacon ID) and include GPS coordinates). One example of a 406 MHz PLB can be seen here but I cannot state that it is the best....just that I am leaning towards this one now: http://www.mcmurdo.co.uk/?Menu=17&Page=/Contents/ListProducts.asp&ID=1026 If I had to make an off-field landing I would activate it in-flight and it is possible that SAR personnel would know of the activation before I made contact with the ground...to include my exact location. A few weeks ago two men were flying around and reported missing. A search was conducted in the south part of the state then after it was found that they had refueled in the north the search moved there. They have not been found and if they survived a crash/off-field landing are now likely deceased. Whether a 406 PLB would have helped is unknown but when the ability to transmit your exact location instantly is now possible and affordable, compared to hours and a large search area for 121.5 Mhz ELTs, I will take advantage of improved technology. Any comments? Ron Lee ________________________________________________________________________________
Date: Apr 24, 2005
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Scud Running
"When you're buzzing along at 175 kts at 1500 AGL under a deck and there's a row 1500 ft high towers in your path." I am not recommending or rebuking, but those who do scud run have some rules. To name a few: Fly slower, may be as slow as 80-90mph with partial flaps as conditions dictate Fly over know terrain that you have flown at low altitudes before in good weather Have the ability to fly IFR legally, otherwise avoid it. The point of the original e-mail is well taken, a GPS with an obstacle / terrain warning feature can be a lifesaver. We had a local young freight pilot fly into a 1700' town flying into the sun. Yes he should have been at the sectional MSA-min safe altitude, but we all like to sight see. I think this feature would be a real plus at night, however 2000' AGL towers are going up all the time. There are no guarantees from Garmin or AWM you will have every obstacle in the database. As a matter of fact a Garmin rep at Oshkosh 2 years ago told me they would never have this feature due to liability and the difficulty in tracking new obstacles. Even Jeppesen has disclaimers on their approach plates. So it is an adjunct. Cheers George ________________________________________________________________________________
Date: Apr 24, 2005
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Emergency notification (Was: RV-6 Crash)
>Linn, the ELT has a G-sensor which the PLB's do not have (the "P" is for >personal). Further you've got the whole TSO/holy water thing to contend >with. And as Jerry noted, we don't need no steeenking 337's for >experimentals. There ARE 406mhz ELT's currently available but they are big >$$$. PLB's may be a good addition but can't replace ELT's. We hashed >through this issue about 4-5 motnths ago. > >Greg Young The PLB is in addition to the ELT and offers substantial improvements over 121.5 MHz ELTs in that it can take the "search" out of Search and Rescue. Here is a link that will explain some of the issues. Additional links are there as well. http://www.sarsat.noaa.gov/emerbcns.html Ron Lee ________________________________________________________________________________
Date: Apr 24, 2005
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Emergency notification (Was: RV-6 Crash)
> >On the flight a few days ago, we were on 122.75 and no ATC. Never again. > > >Not sure why. When I fly, I want to concentrate on the scenery, and >scan for other aircraft. True, flight following or ATC can give you >some separation ..... but not always unless you've filed (from what I >understand). Use of flight following is easy and hardly detracts from enjoying the scenery. I do not "file" anything. Just call up appropriate approach control or center and ask for VFR flight following. Separation is one benefit but the other is immediate help if a problem arises. Ron Lee ________________________________________________________________________________
Date: Apr 24, 2005
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Scud Running
>The point of the original e-mail is well taken, a GPS with an obstacle / >terrain warning feature can be a lifesaver. ..... So it is an adjunct. >Cheers George Just as one software program "could" allow you to fly in the mountains in fog and use the terrain portrayal to avoid hitting cumulus granitus. I would never do that but in a situation where it was that option or certain impact, I would go with the non-approved option. Ron Lee ________________________________________________________________________________
From: Paul Folbrecht <paul.folbrecht(at)VERIBOX.NET>
Subject: QB Questions
Date: Apr 24, 2005
A couple general questions about QB kits. 1) Are there ever problems with getting enough access in the wings for installing autopilot servos, lights, or anything else? I know they come sans one skin only.. is that enough? 2) Any thoughts about the wash primer used? I know some ppl paint the inside of the fuse in addition to that. Why? The wash primer is deemed not sufficient for corrosion protection? ________________________________________________________________________________
From: "Paul Besing" <paul(at)kitlog.com>
Subject: Scud Running
Date: Apr 24, 2005
Good point. When I was doing helicopter training in southern Alabama, a new tower would pop up alot, and would only be on a NOTAM, but not in the charts/gps updates. Again, my original post was NOT to put anyone's skills down, but to simply enlighten those who may not be as cautious while staying under a cloud layer. Personally, I LOVE flying in the clouds. Call it sick, but something about it all working together, and getting to your destination using good training is very rewarding. When the convection activity is low, and all you have is bad visibility, it could be quite fun. Just please be careful out there. We have a great system in place for us to fly actual IFR, so use the tools available! Paul Besing RV-10 Soon Kitlog Builder's Software www.kitlog.com -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Charles Heathco Subject: Re: RV-List: Scud Running Scud running is one thing, trying to fly thru mountainous terrain in the dark another. Nothing wrong with scud running at 1500agl provided you can see all around you and keep an escape route availible. As for me, I keep a current chart open and my finger on my location at all times no matter the altitude. For sure I wouldnt trust any gps to warn me of a tower, for example, a new very high tower has been put up SE of LZU that dosnt show up on the 296. Trying to thread a way thru know towers in low visibility is also not a good thing. charlie heathco ________________________________________________________________________________
From: "Andre Berthet" <aberthet(at)sbcglobal.net>
Subject: Emergency notification (Was: RV-6 Crash)
Date: Apr 24, 2005
I'm planning a trip to Baja California next week and decided to buy a PLB. I got the mcmurdo Fastfind Plus (with internal GPS) from Landfall Navigation http://www.landfallnav.com/index.html for $540.00. It's seems to be a nice and well built instrument. I already registered it online with NOAA SARSAT. As someone eluded before, in case of a crash the Personal Locator Beacon (PLB) will need to be activated manually by the person in distress if he or she is able. Andre Berthet > > > > >Linn, the ELT has a G-sensor which the PLB's do not have (the "P" is for > >personal). Further you've got the whole TSO/holy water thing to contend > >with. And as Jerry noted, we don't need no steeenking 337's for > >experimentals. There ARE 406mhz ELT's currently available but they are > big > >$$$. PLB's may be a good addition but can't replace ELT's. We hashed > >through this issue about 4-5 motnths ago. > > > >Greg Young > > The PLB is in addition to the ELT and offers substantial improvements over > 121.5 MHz ELTs in that it can take the "search" out of Search and Rescue. > ________________________________________________________________________________
From: "Tony Marshall" <tony(at)lambros.com>
Subject: Lyc 0360 w Hartzell Constant Speed
Date: Apr 24, 2005
My question has probably been addressed a 100 times, but I couldnt find it in the archives, so here it is again.... RV6....What are the normal power/performance settings for my engine prop combo? I realize MP is a function of altitude, but would be interested in approximate expected settings (MP, RPM, Fuel Burn) at SL, 3000, 6000, 9000, 12000 for performance cruise 75%, economy cruise 65%. Thanks for your assistance. Tony Marshall RV6 Polson, MT ________________________________________________________________________________
Date: Apr 24, 2005
From: GMC <gmcnutt(at)shaw.ca>
Subject: Scud Running
a new tower would pop up and would only be on a NOTAM, but not in the charts/gps updates. ------------------------------------------------ Question, - anyone on the list know how far towers have to be set back from roads and highways. We don't have that many big towers around here and most that I have noticed on my flights East seem to be set back enough that if they toppled over they would not come down on an adjacent highway. Nice to know for sure if following a highway in poor weather (150 'right of centerline). George in Langley BC 6A flying 7A fuse. ________________________________________________________________________________
From: "Richard Bibb" <rebibb(at)comcast.net>
Subject: Re: QB Questions
Date: Apr 25, 2005
Answer: 1) Yes 2) Yes but as you probably have discovered there are a myriad of opinions on the subject. > > A couple general questions about QB kits. > > 1) Are there ever problems with getting enough access in the wings for > installing autopilot servos, lights, or anything else? I know they > come sans one skin only.. is that enough? > > 2) Any thoughts about the wash primer used? I know some ppl paint the > inside of the fuse in addition to that. Why? The wash primer is > deemed not sufficient for corrosion protection? > ________________________________________________________________________________
From: "Pat Hatch" <pat_hatch(at)msn.com>
Subject: QB Questions
Date: Apr 25, 2005
Paul, I built a QB -7 and there's plenty of access for servos, lights, etc. You may have to get a Unibit extension (Avery sells them) to drill additional wiring holes through the ribs. The problem you will encounter is only on the inboard end of the wing where the ribs are spaced too close together for drilling access. As for the priming, too many variables here...check the archives and make your own decision. My own opinion, the wash primer will be just fine unless you live in a humid or salty area. If the airplane is to be hangared, I wouldn't worry about it. Hope this helps, Pat Hatch RV-6 RV-7 A couple general questions about QB kits. 1) Are there ever problems with getting enough access in the wings for installing autopilot servos, lights, or anything else? I know they come sans one skin only.. is that enough? 2) Any thoughts about the wash primer used? I know some ppl paint the inside of the fuse in addition to that. Why? The wash primer is deemed not sufficient for corrosion protection? ________________________________________________________________________________
From: "Glen Matejcek" <aerobubba(at)earthlink.net>
Subject: Emergency notification (Was: RV-6 Crash)
Date: Apr 25, 2005
Hi All- Something that has been missing from this exchange on ELTs, as well as the linked federal page, is that modern ELTs transmit on both the civil 121.5 AND military 243. Consequently, and although 121.5 is going away, any recent (decades old?) ELT will most likely still be legal / useful until the military comes up with both the motivation and spare cash to convert their equipment to something better. Of course, if good / fast SAR is a concern, one could have 121.5 tuned in Com 2, or a memory slot of the only Com. This could facilitate a couple of things, given that all FSS, ATCT, and I believe all ARTCC's listen in. First, one could listen for other's distress call in order to relay info and help localize another downed airplane. Second, instead of just turning on your own ELT while airborne and announcing to everyone that someone somewhere is in trouble, you could transmit your pan or mayday call to include your present position. Poof, help is on the way. Subsequently, you could turn the ELT on prior to the impact, On the ergonomics side, I have chosen to put the remote head for my ELT adjacent to my battery and IGN switches. This way, I have to look at it each time I shut down. This forces me to check for false activations after a normal arrival as well as reminding me to activate it manually when killing the bats and IGN prior to a forced landing. Soapbox mode off... Glen Matejcek aerobubba(at)earthlink.net ________________________________________________________________________________
Date: Apr 25, 2005
From: Glenn Rainey <nimbusaviation(at)yahoo.com>
Subject: ram air box
Hi RV people. I am a long-EZ (re)builder, and am installing an RV ram air box (FAB) on my O-235 L2C according to the configuration of one of our gurus 'over here' in the canard community. I'd be keen to catch sight of the airbox configuration as it is called out in the RV plans, by way of critique for what we're trying to do here for the plastic airplane. (as an aside, I found some of the holes factory-drilled in the upper filter attach plate to be out of position, so I've re-fabricated that part) I would be very grateful if someone had the chance maybe to scan in a page or 2 of the RV plans so I can see this airbox. Perhaps contact me offlist. Thanks, very much, in anticipation. Glenn Rainey Scotland Long-EZ 'prefurb' ________________________________________________________________________________
Date: Apr 25, 2005
From: John Huft <rv8(at)lazy8.net>
Subject: Re: Emergency notification (Was: RV-6 Crash)
Andre, if you go down in Mexico, no one is going to come looking for you. John Andre Berthet wrote: > >I'm planning a trip to Baja California next week and decided to buy a PLB. I >got the mcmurdo Fastfind Plus (with internal GPS) from Landfall Navigation >http://www.landfallnav.com/index.html for $540.00. It's seems to be a nice >and well built instrument. I already registered it online with NOAA SARSAT. >As someone eluded before, in case of a crash the Personal Locator Beacon >(PLB) will need to be activated manually by the person in distress if he or >she is able. > >Andre Berthet > > > >> >> >> >> >>>Linn, the ELT has a G-sensor which the PLB's do not have (the "P" is for >>>personal). Further you've got the whole TSO/holy water thing to contend >>>with. And as Jerry noted, we don't need no steeenking 337's for >>>experimentals. There ARE 406mhz ELT's currently available but they are >>> >>> >>big >> >> >>>$$$. PLB's may be a good addition but can't replace ELT's. We hashed >>>through this issue about 4-5 motnths ago. >>> >>>Greg Young >>> >>> >>The PLB is in addition to the ELT and offers substantial improvements over >>121.5 MHz ELTs in that it can take the "search" out of Search and Rescue. >> >> >> > > > > ________________________________________________________________________________
Date: Apr 25, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: QB Questions
> Answer: > > 1) Yes Yes, there are problems? What kinds have you run into? With all the people using autopilots these days, I have to believe it's possible to get a servo in there. I can deal with a little extra work. [As long as it doesn't end up negating the time-savings of the QB wing entirely. ;-)] > > 2) Yes but as you probably have discovered there are a myriad of opinions on > the subject. > > > > > > A couple general questions about QB kits. > > > > 1) Are there ever problems with getting enough access in the wings for > > installing autopilot servos, lights, or anything else? I know they > > come sans one skin only.. is that enough? > > > > 2) Any thoughts about the wash primer used? I know some ppl paint the > > inside of the fuse in addition to that. Why? The wash primer is > > deemed not sufficient for corrosion protection? > > > > > > > > > > ________________________________________________________________________________
Date: Apr 25, 2005
From: Ron Lee <ronlee(at)pcisys.net>
Subject: Re: Emergency notification (Was: RV-6 Crash)
>Andre, if you go down in Mexico, no one is going to come looking for you. > >John At least with the PLB, SAR resources will know about you and call the contact numbers they have on file. Ron Lee ________________________________________________________________________________
From: "Tony Marshall" <tony(at)lambros.com>
Subject: Performance Settings RV6 Lyc 0360 w Hartzell Constant Speed
Date: Apr 25, 2005
Repost... My question has probably been addressed a 100 times, but I couldnt find it in the archives, so here it is again.... RV6....What are the normal power/performance settings for my engine prop combo? I realize MP is a function of altitude, but would be interested in approximate expected settings (MP, RPM, Fuel Burn) at SL, 3000, 6000, 9000, 12000 for performance cruise 75%, economy cruise 65%. Thanks for your assistance. Tony Marshall RV6 Polson, MT ________________________________________________________________________________
Subject: Rocket vs RV revisited
Date: Apr 25, 2005
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
SNIP Now, there is no way I would take my plane to CAFE and expect to set any records. From what little I know of John Harmon is that he took his personal plane with no fan fare or special mods and set several CAFE records. Now, (I may get some of this wrong but it is what I heard), the RV-4 was highly modified. It was build very light and not painted to save more weight. Unlike most RVs, I would not want to be in it if acro was being performed. The pilot even lost a lot of weight. I am sure there were many more things done in search of the record book. Let me say, I see nothing wrong in this. But comparing a "Stock" Rocket with a "Special" RV-4 is like comparing apples to oranges. I don't take my car to the race track and expect to compete with formula F-1 cars. Tom Gummo SNIP *************************************************************************** I would add that Bruce Bohannon is using a Rocket to set his altitude records, albeit with a much larger wing. I don't understand why he calls it a "highly modified RV-4." Maybe to cheese Van a bit, maybe he had a falling out with the well-known Rocket builder who built it, I don't know. It is definitely "Rocketized." Looking at this another way, hmmmm, maybe we're all just flying highly modified Stits products?????? It would be VERY interesting if Dave Anders prepped a Rocket for the CAF competition. Maybe it wouldn't do as well, but it would be VERY interesting nonetheless. My apologies to those who thought my analogy about the supermodels wasn't accurate. I confess, it's true.... I've never actually had 12 Victoria Secret models fighting over me. OTOH, I'll wager that those who didn't understand my analogy have never flown a Rocket, and those who do fly Rockets fully understand the analogy and know that it's as close to the truth as can be explained in verbal terms. I strongly suspect that Spaceship One, the X-15, and a very few other aircraft, none of which we mere mortals are likely to ever fly, can beat the Rocket for sheer fun. That's the rub with the Rocket, and the RV's too, mere mortals can build them, fly them, and still send the kids to college with what's left. Please don't ever think that I'm knocking the RVs, just stating that there is something else beyond "Total Performance." Vince ________________________________________________________________________________
From: LeastDrag93066(at)aol.com
Date: Apr 25, 2005
Subject: 70" Hartzell?
Hi All, Is anyone running a 70" dia. Hartzell 7666A4 propeller on their Lycoming O-360-A1A engine? Preferably for three years, or more. A friend with a RV-6 had a little mishap which shortened his 72" dia. Hartzell to about a 70" dia. BTW, I already know that 72" is the minimum acceptable length for this propeller, so we don't need to start that thread. :-) Regards, Jim Ayers ________________________________________________________________________________
From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com>
Subject: Airflow Performance fuel pump
Date: Apr 25, 2005
I feel a little stupid about admitting my situation , but hopefully this post will save someone else some time. I am using the Airflow Performance fuel pump (purchased from Van's) and it is all installed, plumbed and wired... I tested the wires for continuity to the switch, everything was good until I put power to the pump to momentarily test for function...then, NOTHING happened. I rechecked voltage through the wires and through the switch, then with power coming from the switch, I measured voltage across the pump terminals to verify power was making it from the switch...yep. I called Don at AFP and he said "send it in"...perfect...now just to stand on my head, pull off the cover plates, enjoy the reverse plumbing job, undo the wiring, box it up, drive to UPS, ship it, and wait... Long story short... BENCH TEST THE PUMP BEFORE INSTALLING IT. Bob Brown RV-7A wiring ________________________________________________________________________________
From: LeastDrag93066(at)aol.com
Date: Apr 25, 2005
Subject: Lyc. 360 - Hartzell vs. MT aluminum 2 blade
Hi All, This information is specifically applicable to the Lycoming 360 non-counterweighted crankshaft engines. Van's Aircraft sells 72" and 74" diameter 2 blade CS Hartzell propellers. The aluminum 2 blade CS MT propeller (MTV-15-B/183-402) has a 72" diameter. In the case of blade damage, the Hartzell minimum blade diameter is 72". (So don't damage your 72" dia. Hartzell.) In the case of blade damage, the MTV-15-B/183-402 minimum blade diameter is 68". On a stock Lyc. 360 engine; The Hartzell /F766xxx propeller has a RPM restriction between 2000 to 2250 RPM for continuous operation. The Hartzell /F7496( ) propeller does not have RPM restrictions for the 180 hp Lyc. On the 200 hp Lyc., this propeller has a RPM restriction between 2000 to 2250 RPM for continuous operation. The MTV-15-B/183-402 does not have RPM restrictions. On an aftermarket electronic ignition, LASAR system, or FADEC system equipped Lyc. 360 engine; The Hartzell /F766xxx propeller has a RPM restriction between 2000 to 2250 RPM for continuous operation and a maximum continuous operating limitation of 2600 RPM. The Hartzell /F7496( ) propeller cannot be operate above 22" MP below 2350 RPM. There is a maximum continuous operating limitation of 2600 RPM. The maximum takeoff RPM is limited to 2650 RPM for FADEC equipped engines. The MTV-15-B/183-402 does not have RPM restrictions. For a Lyc. 360 engine with high compression pistons and an aftermarket electronic ignition, LASAR system, or FADEC system; Hartzell recommends that you do not use their propeller. The MTV-15-B/183-402 does not have RPM restrictions. Van sells the aluminum 2 blade CS Hartzell 72" dia. /F766xxx propellers for $5,420, and the /F7496( ) propellers for $5,650. The spinner costs extra, the rear bulkhead has to be trimmed to fit the hub and the spinner dome has to be fitted to the propeller blades. Less Drag Products, Inc, MT Propeller USA, Inc. and MT Propeller sell the aluminum 2 blade CS MT 72" dia. propeller for $6,399. The bulkheads are mounted on the propeller hub with a painted (or primed) completed spinner dome. Basically, the propeller/spinner assembly comes ready to bolt onto your engine with a 1/4" spinner clearance to the cowl. The bottom line: If you are putting together an RV with a stock Lyc. 360 engine, the 72" dia. 2 blade Hartzell can make a great package. If your RV Lyc. 360 engine is a stock 200 hp, or has a little extra something, then consider the MTV-15-B/183-402 propeller. Regards, Jim Ayers Less Drag Products, Inc. _www.lessdrag.com_ (http://www.lessdrag.com) (805) 795-5377 Prices subject to change without notice. ________________________________________________________________________________
From: "Don Kugler" <donkugler(at)earthlink.net>
Subject: RV8/8As being built near KLOM?
Date: Apr 25, 2005
Anyone in the vicinity of Wings Field (KLOM) with an RV8 or -8A under construction? I've got a friend who lives in that area that I recently took for a ride in my -8 and he's hooked - no surprise. He would like to see one in the construction phase. Please respond off-list. Thanks, -Don Don Kugler donkugler(at)earthlink.net RV8 @ N40 ________________________________________________________________________________
Date: Apr 25, 2005
From: Walter Tondu <walter(at)tondu.com>
Subject: Re: Airflow Performance fuel pump
On 04/25 10:58, Karen and Robert Brown wrote: > > I feel a little stupid about admitting my situation , but hopefully this post will save someone else some time. I am using the Airflow Performance fuel pump (purchased from Van's) and it is all installed, plumbed and wired... > > I tested the wires for continuity to the switch, everything was good until I put power to the pump to momentarily test for function...then, NOTHING happened. I rechecked voltage through the wires and through the switch, then with power coming from the switch, I measured voltage across the pump terminals to verify power was making it from the switch...yep. > > I called Don at AFP and he said "send it in"...perfect...now just to stand on my head, pull off the cover plates, enjoy the reverse plumbing job, undo the wiring, box it up, drive to UPS, ship it, and wait... > > Long story short... BENCH TEST THE PUMP BEFORE INSTALLING IT. Even if you bench test it, there can be Gremlins. Mine didn't work the first time I flipped the switch, it kept blowing 10A fuses. Tested everything, wiring checked out perfectly. Put the pump on the bench and it ran, put it back in and it didn't. Got confused as hell. Sent the pump in to get diagnosed. It was fine. Turns out one of my expensive switches was bad. Go figure. -- Walter Tondu http://www.rv7-a.com ________________________________________________________________________________
From: "LARRY ADAMSON" <rvhi03(at)msn.com>
Subject: Re: QB Questions
Date: Apr 25, 2005
----- Original Message ----- From: Paul Folbrecht Subject: Re: RV-List: QB Questions If the QB wing is not skinned on both sides by the aileron bell crank inspection opening, then the auto-pilot servo is easy to install. In can also be installed in a finished wing, but a much tougher process. I'm at that point right now, and will probably go with an installation that puts the servo in the wing tip. Very easy to do on a finished wing, but ends up slightly heavier due to a pushrod that needs to be at least 3/4" diameter and around 57" long. I'll just put it in the right wing (RV6A) to offset my own weight on solo flight. Inside wing installations use pushrods that are only about 6-8" long. IMO ---- Two very good A/Ps are the TruTrak and the Trio EZ Pilot. Both use a panel mounted or newer handheld GPS for heading information. Altitude A/P's can easily be installed anytime. Using the search function for either of these A/P's, you can get diagrams. Other pics are also on the net. ________________________________________________________________________________
Subject: BMA EFIS Light
Date: Apr 25, 2005
From: "Valovich, Paul" <pvalovich(at)dcscorp.com>
When I called Blue Mountain Avionics last week to inquire about their EFIS Light, I was told 85 units had already been shipped. Does anyone have any comments regarding installation / operation / reliability? What about the autopilot option? Paul Valovich RV-8A QB Delivery Thursday ________________________________________________________________________________
Date: Apr 25, 2005
From: sportav8r(at)aol.com
Subject: Anyone have a comparison of Garmin 296 and iQue3600a?
Looking for a nice color GPS with terrain, obstacles & VNAV, capable of driving a Trio A/P. I know the 296 fits the bill nicely, but I'm wondering what the 296 offers that makes it worth $400 more than the iQue 3600a Palm offering form Garmin. They have the same screen resolution and size (one is portrait orientation, the other landscape, I suppose) but the PDA doubles as, well, a PDA. As a long time Handspringt and Palm user, I am trying to find the downside to owning a nice Palm that does everything I want a handheld aviation GPS to do, versus a dedicated aviation GPS for 400 bucks more that will not do much for me outside the airplane. Am I missing something here? What are the Palm's shortcomings? There must be something... -Stormy ________________________________________________________________________________
Date: Apr 25, 2005
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Scud Running
GMC wrote: > > >a new tower would pop up and would only be on a NOTAM, but not in the >charts/gps updates. >------------------------------------------------ >Question, - anyone on the list know how far towers have to be set back from >roads and highways. We don't have that many big towers around here and most >that I have noticed on my flights East seem to be set back enough that if >they toppled over they would not come down on an adjacent highway. Nice to >know for sure if following a highway in poor weather (150 'right of >centerline). > >George in Langley BC >6A flying >7A fuse. > Around here there isn't enough 'wiggle room' to make me trust myself to remain between them while trying to follow curves in the road, communicate, read the chart, etc. If it's a 600' tower & it's 700' off the road, that ain't much room. In the US, cell towers are *everywhere*. A few years ago they tried to put a 600' cell tower directly on the extended centerline of my home strip (MS71) 3 miles from the numbers (about a thousand feet from the highway). Charlie ________________________________________________________________________________
From: "LARRY ADAMSON" <rvhi03(at)msn.com>
Subject: Re: Anyone have a comparison of Garmin 296 and iQue3600a?
Date: Apr 25, 2005
----- Original Message ----- From: sportav8r(at)aol.com Subject: RV-List: Anyone have a comparison of Garmin 296 and iQue3600a? From everything I've heard/read, the iQue 3600 has "no" data output for the auto-pilot. I was in the same dilemma & ended up with the 296 for my Trio. The 296 will require a power/data cable which is about $30.00 Of course when I purchased my Garmin, it was $200.00 more! Looking for a nice color GPS with terrain, obstacles & VNAV, capable of driving a Trio A/P. I know the 296 fits the bill nicely, but I'm wondering what the 296 offers that makes it worth $400 more than the iQue 3600a Palm offering form Garmin. They have the same screen resolution and size (one is portrait orientation, the other landscape, I suppose) but the PDA doubles as, well, a PDA. As a long time Handspringt and Palm user, I am trying to find the downside to owning a nice Palm that does everything I want a handheld aviation GPS to do, versus a dedicated aviation GPS for 400 bucks more that will not do much for me outside the airplane. Am I missing something here? What are the Palm's shortcomings? There must be something... -Stormy ________________________________________________________________________________
Date: Apr 25, 2005
From: David Leonard <wdleonard(at)gmail.com>
Subject: Re: BMA EFIS Light
I have one (the EFIS G3 Lite), I like it alot and use it in IMC, however that is only because I have a backup eletric AI (I use the blumountain in HSI mode while in IMC). It does have some drift that I think the company will work out. The moving map is next to worthless right now, but will be improved. But the HSI is the best, brightest and most usefule you can get for less than $10k, and it is only $2.7k Dave Leonard On 4/25/05, Valovich, Paul wrote: > > When I called Blue Mountain Avionics last week to inquire about their > EFIS Light, I was told 85 units had already been shipped. Does anyone > have any comments regarding installation / operation / reliability? What > about the autopilot option? > > Paul Valovich > > RV-8A QB Delivery Thursday > > -- Wm. David Leonard ________________________________________________________________________________
Date: Apr 25, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: QB Questions
Yeah, my panel is a ways away but if I did it today it would be a GRT 2-3 screen system and TruTrak 2-axis AP. Do not achive. > IMO ---- Two very good A/Ps are the TruTrak and the Trio EZ Pilot. Both use a > panel mounted or newer handheld GPS for heading information. Altitude A/P's > can easily be installed anytime. Using the search function for either of > these A/P's, you can get diagrams. Other pics are also on the net. ________________________________________________________________________________
Date: Apr 25, 2005
From: David Leonard <wdleonard(at)gmail.com>
Subject: Re: BMA EFIS Light
Yes, you hit the nail on the head. But if you call it a Beta version it might sit easier. They are usually good about providing the updates to the beta test recipients... like me in this case. None the less I am glad to have it.... Its a great insturment even without any future upgrades (brighter and more versitile than the dynon. Dave Leonard > Dave, > > When you say the moving map is next to worthless and that BMA is still > working on drift issues with the product, does this seem to be a > continuation of BMA's fundamental problem - releasing product before it is > fully developed? > > KB > ----- Original Message ----- > From: "David Leonard" <wdleonard(at)gmail.com> > To: > Sent: Monday, April 25, 2005 10:03 PM > Subject: Re: RV-List: BMA EFIS Light > > > > > I have one (the EFIS G3 Lite), I like it alot and use it in IMC, > > however that is only because I have a backup eletric AI (I use the > > blumountain in HSI mode while in IMC). It does have some drift that I > > think the company will work out. The moving map is next to worthless > > right now, but will be improved. > > > > But the HSI is the best, brightest and most usefule you can get for > > less than $10k, and it is only $2.7k > > > > Dave Leonard > > > > On 4/25/05, Valovich, Paul wrote: > >> > >> When I called Blue Mountain Avionics last week to inquire about their > >> EFIS Light, I was told 85 units had already been shipped. Does anyone > >> have any comments regarding installation / operation / reliability? What > >> about the autopilot option? > >> > >> Paul Valovich > >> > >> RV-8A QB Delivery Thursday > >> > >> > > > > > > -- > > Wm. David Leonard > > > > > > > > > > > > > > > > -- Wm. David Leonard ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Anyone have a comparison of Garmin 296 and iQue3600a?
Date: Apr 25, 2005
I haven't looked too close, but I thought the iQue lacked the output to drive the AP. No? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > From: sportav8r(at)aol.com [mailto:sportav8r(at)aol.com] > Sent: Monday, April 25, 2005 9:13 PM > To: rv-list(at)matronics.com > Subject: RV-List: Anyone have a comparison of Garmin 296 and > iQue3600a? > > > Looking for a nice color GPS with terrain, obstacles & VNAV, > capable of driving a Trio A/P. I know the 296 fits the bill > nicely, but I'm wondering what the 296 offers that makes it > worth $400 more than the iQue 3600a Palm offering form > Garmin. They have the same screen resolution and size (one > is portrait orientation, the other landscape, I suppose) but > the PDA doubles as, well, a PDA. As a long time Handspringt > and Palm user, I am trying to find the downside to owning a > nice Palm that does everything I want a handheld aviation GPS > to do, versus a dedicated aviation GPS for 400 bucks more > that will not do much for me outside the airplane. Am I > missing something here? What are the Palm's shortcomings? > There must be something... > > -Stormy > > > Photoshare, and much much more: > > > > > > ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: Apr 25, 2005
Subject: Advice on using an off-set rivet set
Hi folks I have a single universal head -6 rivet to set. An offset set gives me a much better angle to get to it. However, when I tried to use the thing in my practice piece, it rotated and jumped and was generally nearly impossible to control. Is there a trick to this? Regards, Michael Wynn RV-8, Empennage San Ramon, California ________________________________________________________________________________
From: "Brian Kraut" <brian.kraut(at)engalt.com>
Subject: BMA EFIS Light
Date: Apr 25, 2005
I thought I was going to get the BMA EFIS Lite until I saw just how useless the moving map was at Sun and Fun. The idea of having to pay to update that useless database also didn't appeal to me. Now I am leaning towards the GRT unit and a color handheld with a real moving map. As the GRT people also pointed out, the moving map in the BMA unit can't be used while using the AI which makes it even more useless in IFR. Brian Kraut Engineering Alternatives, Inc. www.engalt.com ________________________________________________________________________________
Date: Apr 25, 2005
From: Ron Lee <ronlee(at)pcisys.net> iQue3600a?
Subject: Anyone have a comparison of Garmin 296 and
iQue3600a? >I haven't looked too close, but I thought the iQue lacked the output to >drive the AP. No? If you check the specs it mentions RS232 so it MAY have the right output but should be checked first. Ron Lee ________________________________________________________________________________
From: owner-rv-list-server(at)matronics.com
Subject: Advice on using an off-set rivet set
Date: Apr 26, 2005
The only reason that a rivet gun will jump on you is that the force pushing it down onto the rivet head does not counteract the kickback. This can be caused by either too much air pressure or your just being inattentive and thereby slacking off. Since you say that the gun jumps on your practice tests, therefore attention not being an issue, I would presume that your pressure is way too high. I mounted a small regulator (Avery) right on my 3X gun and adjust by feel - less pressure for 3/32" rivets than for the 1/8" - don't ask me what the pressure is - I don't know - and it is a moot issue - the real concern is that it should be the right pressure to do the job. Michle RV8 - Fuselage > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of MLWynn(at)aol.com > Sent: Tuesday, April 26, 2005 5:01 AM > To: rv-list(at)matronics.com > Subject: RV-List: Advice on using an off-set rivet set > > > Hi folks > > I have a single universal head -6 rivet to set. An offset set gives me a > much better angle to get to it. However, when I tried to use the thing in > my > practice piece, it rotated and jumped and was generally nearly impossible > to > control. Is there a trick to this? > > Regards, > > Michael Wynn > RV-8, Empennage > San Ramon, California > > > > > ________________________________________________________________________________
From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net>
Subject: Advice on using an off-set rivet set
Date: Apr 26, 2005
> Hi folks > > I have a single universal head -6 rivet to set. An offset > set gives me a > much better angle to get to it. However, when I tried to use > the thing in my > practice piece, it rotated and jumped and was generally > nearly impossible to > control. Is there a trick to this? > > Regards, > > Michael Wynn > RV-8, Empennage > San Ramon, California I NEVER found a way to make an offset rivet set work. Use a pop rivet or bolt. I actually took a torch to mine and straightened it out, as I found that a long set worked much better than trying to use the offset one. Some of the repliers to your question may have missed the "offset" part. Alex Peterson RV6-A 611 hours Maple Grove, MN http://www.home.earthlink.net/~alexpeterson/ ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Apr 26, 2005
Subject: Re: Advice on using an off-set rivet set
In a message dated 4/25/05 10:04:12 PM Central Daylight Time, MLWynn(at)aol.com writes: > I have a single universal head -6 rivet to set. An offset set gives me a > much better angle to get to it. However, when I tried to use the thing in > my > practice piece, it rotated and jumped and was generally nearly impossible to > > control. Is there a trick to this? >>> Taping the set/spring to the gun with aviation grade duct tape will keep the set from rotating. I have even removed the spring and just wrapped tape around the set to the gun barrel for them really tight spots & it worked well enough. This proved very helpful for those pesky wing nose ribs. As others have mentioned, pressure should be as low as needed to set the rivet. Many listers have sung the merits of various cloth-based tapes used on the end of the set (go to RV archives, search for "rivet & tape & hockey", grab a beer or two, and enjoy the long read!) Plus, judicious use of concentration (focus, Luke- use the force!) is occasionally required. Mark Phillips ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Apr 26, 2005
Subject: Re: Advice on using an off-set rivet set
In a message dated 4/25/05 10:04:12 PM Central Daylight Time, MLWynn(at)aol.com writes: > I have a single universal head -6 rivet to set. An offset set gives me a > much better angle to get to it. However, when I tried to use the thing in > my > practice piece, it rotated and jumped and was generally nearly impossible to > > control. Is there a trick to this? >>> Taping the set/spring to the gun with aviation grade duct tape will keep the set from rotating. I have even removed the spring and just wrapped tape around the set to the gun barrel for them really tight spots & it worked well enough. This proved very helpful for those pesky wing nose ribs. As others have mentioned, pressure should be as low as needed to set the rivet. Many listers have sung the merits of various cloth-based tapes used on the end of the set (go to RV archives, search for "rivet & tape & hockey", grab a beer or two, and enjoy the long read!) Plus, judicious use of concentration (focus, Luke- use the force!) is occasionally required. Mark Phillips ________________________________________________________________________________
Date: Apr 26, 2005
From: rv6fly <rv6fly(at)bresnan.net>
Subject: Re: Advice on using an off-set rivet set
MLWynn(at)aol.com wrote: > >Hi folks > >I have a single universal head -6 rivet to set. An offset set gives me a >much better angle to get to it. However, when I tried to use the thing in my >practice piece, it rotated and jumped and was generally nearly impossible to >control. Is there a trick to this? > > You've received good advice so far. I'd think along the lines of too much pressure, too light of a bucking bar. Swivel sets are a bit more difficult to use but can be mastered. Make sure your work is secured. If you have to spend energy and attention on trying to control your practice piece, the end results won't be very good. Also, try some masking tape in the cupped face of the set. Masking tape on the factory head of the rivet would be a second choice. Let everyone know if any of the suggestions work for you. Bob Skinner ________________________________________________________________________________
From: LeastDrag93066(at)aol.com
Date: Apr 26, 2005
Subject: Re: RV-List Performance Settings RV6 Lyc 0360 w Hartzell Constant
Speed Hi Tony, For the Hartzell CS propeller on the Lyc. 360 engine at 7,500' and above, 2300 RPM and full throttle for maximum speed with best fuel economy. Since the propeller pulls the aircraft through the air, and not the engine, you asked a good question. I have posted a chart of power settings, airspeeds and fuel flow at _www.lessdrag.com_ (http://www.lessdrag.com) on the "Lycoming 360 Propeller" page. You can see the performance trends on this chart taken on a RV-6A. Regards, Jim Ayers In a message dated 04/26/2005 2:31:04 AM Pacific Daylight Time, rv-list-digest(at)matronics.com writes: --> RV-List message posted by: "Tony Marshall" Repost... My question has probably been addressed a 100 times, but I couldnt find it in the archives, so here it is again.... RV6....What are the normal power/performance settings for my engine prop combo? I realize MP is a function of altitude, but would be interested in approximate expected settings (MP, RPM, Fuel Burn) at SL, 3000, 6000, 9000, 12000 for performance cruise 75%, economy cruise 65%. Thanks for your assistance. Tony Marshall RV6 Polson, MT ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: Advice on using an off-set rivet set
Date: Apr 26, 2005
I disagree with Peterson's response on this. (sorry if this hurts your feelings but it is the truth -- my apologies). The offset works just fine if you know how to use it. You need to have good control of the piece you are working with. Strap or vice grip it down if it is not enough mass to be solid enough and steady to absorb the riveting when it occurs with out moving. No one can rivet a moving target. Keep steady and solid pressure on the rivet gun. It must be enough pressure that it will not bounce off the rivet. Keep your angle perfect at 90 degrees. Keep the bucking bar on it. You could start with lower pressure and adjust up if it is not setting the rivet with a 1 second burst. Summary: Most important is controlling the piece you are working on, then keep your gun on the rivet. Works for me. Don't use pop rivets unless you want to reduce the strength the plane designer had in mind. By the time you realize that a parent was right, there is a child who thinks you're wrong. Indiana Larry, RV7 Tip Up FLYING - Phase 1 ----- Original Message ----- From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net> Subject: RE: RV-List: Advice on using an off-set rivet set > > > >> Hi folks >> >> I have a single universal head -6 rivet to set. An offset >> set gives me a >> much better angle to get to it. However, when I tried to use >> the thing in my >> practice piece, it rotated and jumped and was generally >> nearly impossible to >> control. Is there a trick to this? >> >> Regards, >> >> Michael Wynn >> RV-8, Empennage >> San Ramon, California > > I NEVER found a way to make an offset rivet set work. Use a pop rivet or > bolt. I actually took a torch to mine and straightened it out, as I found > that a long set worked much better than trying to use the offset one. > Some > of the repliers to your question may have missed the "offset" part. > > Alex Peterson > RV6-A 611 hours > Maple Grove, MN > > http://www.home.earthlink.net/~alexpeterson/ > > > ________________________________________________________________________________
Date: Apr 26, 2005
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: Advice on using an off-set rivet set
Michael, I found it best to have a helper to buck the rivet, as I always needed my other hand to hold the double offset. Charlie Kuss > >Hi folks > >I have a single universal head -6 rivet to set. An offset set gives me a >much better angle to get to it. However, when I tried to use the thing in >my >practice piece, it rotated and jumped and was generally nearly impossible to >control. Is there a trick to this? > >Regards, > >Michael Wynn >RV-8, Empennage >San Ramon, California > > ________________________________________________________________________________
From: owner-rv-list-server(at)matronics.com
Subject: Advice on using an off-set rivet set
Date: Apr 26, 2005
Beg to differ - I have used the offset on 470 1/8" rivets near ribs - no problem - trick is to push straight down on the gun, not towards the rivet. Michle RV8 - Fuselage > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of Alex & Gerry Peterson > Sent: Tuesday, April 26, 2005 1:42 PM > To: rv-list(at)matronics.com > Subject: RE: RV-List: Advice on using an off-set rivet set > > > > > > Hi folks > > > > I have a single universal head -6 rivet to set. An offset > > set gives me a > > much better angle to get to it. However, when I tried to use > > the thing in my > > practice piece, it rotated and jumped and was generally > > nearly impossible to > > control. Is there a trick to this? > > > > Regards, > > > > Michael Wynn > > RV-8, Empennage > > San Ramon, California > > I NEVER found a way to make an offset rivet set work. Use a pop rivet or > bolt. I actually took a torch to mine and straightened it out, as I found > that a long set worked much better than trying to use the offset one. > Some > of the repliers to your question may have missed the "offset" part. > > Alex Peterson > RV6-A 611 hours > Maple Grove, MN > > http://www.home.earthlink.net/~alexpeterson/ > > > > > ________________________________________________________________________________
From: "Karen and Robert Brown" <bkbrown(at)ashcreekwireless.com>
Subject: Re: Advice on using an off-set rivet set
Date: Apr 26, 2005
Hey Michael, I'm in agreement with John Starn...gun control means using both hands...adjust your air pressure correctly and, when you use the offset, hold the rivet set with your "off" hand while riveting if possible. If it's not possible to steady the set with your other hand, sometimes you can sort of push or pull the gun sideways depending on which direction you want the set to be when you begin riveting. Using the offset is kinda like a crosswind landing...you have to keep track of lots of things at the same time. Bob Brown RV7A - wiring ________________________________________________________________________________
From: "Barry Chapman" <bcrnfnps(at)swoi.net>
Subject: Re: Advice on using an off-set rivet set
Date: Apr 26, 2005
Hi all, It took me a while to find it, but I came across an old post on the RV-4 list (even shows photos):Sep 28 2003 Henry Hore Rivet-gun double off-set holder for one hand opera... RV4 It looks like it would work/help. Please let us know if you decide to build one and how it works. Thanks Barry Chapman Just a wishin' and dreamin' ----- Original Message ----- From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net> Subject: RE: RV-List: Advice on using an off-set rivet set >> Hi folks >> >> I have a single universal head -6 rivet to set. An offset >> set gives me a >> much better angle to get to it. However, when I tried to use >> the thing in my >> practice piece, it rotated and jumped and was generally >> nearly impossible to >> control. Is there a trick to this? >> >> Regards, >> >> Michael Wynn >> RV-8, Empennage >> San Ramon, California > > I NEVER found a way to make an offset rivet set work. Use a pop rivet or > bolt. I actually took a torch to mine and straightened it out, as I found > that a long set worked much better than trying to use the offset one. > Some > of the repliers to your question may have missed the "offset" part. > > Alex Peterson > RV6-A 611 hours > Maple Grove, MN > > http://www.home.earthlink.net/~alexpeterson/ > > > ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Apr 26, 2005
Subject: Re: Advice on using an off-set rivet set
In a message dated 4/25/05 8:04:09 PM Pacific Daylight Time, MLWynn(at)aol.com writes: > I have a single universal head -6 rivet to set. An offset set gives me a > much better angle to get to it. However, when I tried to use the thing in > my > practice piece, it rotated and jumped and was generally nearly impossible to > control. Is there a trick to this? > > Mike: Masking tape in the cup of the set helps, but the best solution is to > have someone else buck so that you can stabilize the set with two hands. > Good luck. > > Harry Crosby > RV-6 N16CX, 68 hours. ________________________________________________________________________________
From: "Bob Hodgson" <bob(at)hodgson252.freeserve.co.uk>
Subject: Re:Advice on using an off-set rivet set
Date: Apr 26, 2005
Mike, Offset rivet sets do try to rotate unless you duct tape them to the gun at around 45 deg, and/or restrain them with your other hand. Unless you're over-endowed with hands, this may mean an assistant on the bucking bar! Is this an AN470AD6-x or an AN470AD4-6 ? If it's a 3/16 diameter rivet, you need a lot of pressure and at least a 4X gun, so it will need a VERY firm grip to control it. Try leaning on it as you squeeze the trigger, and get your assistant to allow the bar to bounce a little on the shop head rather than hold it immovably against it. FWIW, I use 35 psi for 3/32 and 45 for 1/8 (measured at the compressor). Haven't had to do any 3/16, but would try 55 for a start, or buy a big squeezer. Good Luck, Bob (UK) RV3B (still 'finishing' . . ) ----- Original Message ----- > > From: MLWynn(at)aol.com > Subject: RV-List: > > > Hi folks > > I have a single universal head -6 rivet to set. An offset set gives me a > much better angle to get to it. However, when I tried to use the thing in my > > practice piece, it rotated and jumped and was generally nearly impossible to > control. Is there a trick to this? > > Regards, > > Michael Wynn > RV-8, Empennage > San Ramon, California ________________________________________________________________________________
From: "Jeff Dowling" <shempdowling2(at)earthlink.net>
Subject: Re: Aft Skirts
Date: Apr 26, 2005
The RV-ator has a trick. It talks about notching your first piece so you can get an exact fit, then riveting a second thin piece to the first. Shemp/Jeff Dowling RV-6A, N915JD 190 hours Chicago/Louisville ----- Original Message ----- From: "Pete Howell" <pete.howell@gecko-group.com> Subject: RV-List: Aft Skirts > > Hello, > > Anybody have any neat tricks to get the proper curve in the aft slider > skirts? I have the tops nailed, but the twist along the bottom part is > vexing. > > Cheers, > > Pete Howell > > > ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: Apr 26, 2005
Subject: Re: Advice on using an off-set rivet set
This is all good advice. Thanks to all for taking the time. Regards, Michael Wynn RV8 Empennage ________________________________________________________________________________
From: "Mike D'Ambrogia" <miked(at)jamagination.com>
Subject: Anybody in the 209 need help ?
Date: Apr 26, 2005
All, Like to see what bucking rivets is all about before I get too deep into fantasizing about a -7/-8. If somebody in the 209 area code needs a warm body to help out let me know Thanks Mike ________________________________________________________________________________
From: "Bob 1" <rv3a.1(at)comcast.net>
Subject: Re: Scud Running
Date: Apr 26, 2005
For a crop duster close to home 200 and a mile might be perfectly safe. For a flat-lander in the mountains 3000 and 10 might be suicide. It all depends, and it is really about risk management. John and Martha King have a good CD out about risk management. It is well worth watching and might get you a discount on your insurance. Tailwinds, Doug Rozendaal --------------------------- Speaking as a crop duster... 200 and a mile from home is as safe as CAVU. If anybody knows of an insurance company currently offering a discount for taking the King thing, please point me in the direction. Bob ________________________________________________________________________________
From: "Mike Holland" <hollandm(at)pacbell.net>
Subject: Flluroescent Light Tach Calibration
Date: Apr 26, 2005
I know that I've read someplace that you can calibrate a tach using a 60hz fluorescent light. Can anyone give me the two blade rpms that will stop the prop? I need to calibrate a tach. Thanks Mike Holland ________________________________________________________________________________
Date: Apr 26, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: Aft Skirts
And which issue might that be? "Jeff Dowling" The RV-ator has a trick. It talks about notching your first piece so you can get an exact fit, then riveting a second thin piece to the first. Shemp/Jeff Dowling RV-6A, N915JD 190 hours Chicago/Louisville ----- Original Message ----- From: "Pete Howell" Subject: RV-List: Aft Skirts > > Hello, > > Anybody have any neat tricks to get the proper curve in the aft slider > skirts? I have the tops nailed, but the twist along the bottom part is > vexing. > > Cheers, > > Pete Howell > > > Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) --------------------------------- ________________________________________________________________________________
From: "Vincent Osburn" <flyby41(at)earthlink.net>
Subject: Flluroescent Light Tach Calibration
Date: Apr 26, 2005
I know a fluorescent light flashes 60 times a second or 3600 times a minute or in other words 60 cycles as electricty is produced. Pointing an optical tach at a flourescent light is a fair way to calibrate the tach at 3600 RPM's but I don't know how it would relate to a two bladed prop? Maybe the blade would appear to stop in some division of 3600 RPM's, at 1800 RPM's perhaps or maybe at 900 R's? > [Original Message] > From: Mike Holland <hollandm(at)pacbell.net> > To: > Date: 4/26/2005 8:10:16 PM > Subject: RV-List: Flluroescent Light Tach Calibration > > > I know that I've read someplace that you can calibrate a tach using a 60hz fluorescent light. Can anyone give me the two blade rpms that will stop the prop? I need to calibrate a tach. > > Thanks > > > Mike Holland > > ________________________________________________________________________________
Date: Apr 27, 2005
From: "Richard E. Tasker" <retasker(at)optonline.net>
Subject: Re: Flluroescent Light Tach Calibration
Unless I am mistaken the lowest is 3600 RPM. Fluorescent lights flash at a 120 Hz rate (twice the line rate since there are two peaks per cycle). This is 8.33 milliseconds between peaks. For the propeller to go halfway around so the alternate blade is in the same position in that time, it has to be rotating at 3600 RPM. That is 60 RPS or 16.66 milliseconds all the way around or 8.33 milliseconds halfway around. It is also too fast. You can also use 1800 RPM and the prop would look "stopped", but then you would see four blades because the prop would rotate only 90 degrees between peaks. This is a safer (and attainable) RPM. Likewise you can use proportionally lower RPMs and "see" even more blades. Basically, calculate how far around the prop will go in 8.33 milliseconds for any RPM and see if the blades would look "stopped". For example at 1200 RPM it takes the prop 50 milliseconds for one revolution of the prop. During that time, the lights will peak 50/8.33 = 6 times, which means that the prop rotates 60 per flash. That means you will "see" six blades. At 2400 RPM it takes 25 milliseconds which gives three times or 120 per flash. This will also look like 6 blades. Hopefully this hasn't confused you more than helped. There are lots of RPMs where the blades will look stopped - just depends on how many "blades" you want to see. All of the above is applicable to two blade props only, although the analysis is similar for other numbers. Dick Mike Holland wrote: > >I know that I've read someplace that you can calibrate a tach using a 60hz fluorescent light. Can anyone give me the two blade rpms that will stop the prop? I need to calibrate a tach. > >Thanks > > >Mike Holland > > > > -- ---- Please Note: No trees were destroyed in the sending of this message. We do concede, however, that a significant number of electrons may have been temporarily inconvenienced. ---- ________________________________________________________________________________
From: "Chris & Kellie Hand" <ckhand(at)earthlink.net>
Subject: Re: Advice on using an off-set rivet set
Date: Apr 26, 2005
I have had similar trouble with the offset rivet set, but turning the pressure down a little, practicing, and being real careful with my grip on the gun and bucking bar has usually worked for me. Still is easier with the straight set.... Chris Hand RV-6A, finishing kit ----- Original Message ----- From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net> Subject: RE: RV-List: Advice on using an off-set rivet set > > > > Hi folks > > > > I have a single universal head -6 rivet to set. An offset > > set gives me a > > much better angle to get to it. However, when I tried to use > > the thing in my > > practice piece, it rotated and jumped and was generally > > nearly impossible to > > control. Is there a trick to this? > > > > Regards, > > > > Michael Wynn > > RV-8, Empennage > > San Ramon, California > > I NEVER found a way to make an offset rivet set work. Use a pop rivet or > bolt. I actually took a torch to mine and straightened it out, as I found > that a long set worked much better than trying to use the offset one. Some > of the repliers to your question may have missed the "offset" part. > > Alex Peterson > RV6-A 611 hours > Maple Grove, MN > > http://www.home.earthlink.net/~alexpeterson/ > > ________________________________________________________________________________
From: RSamuelson(at)aol.com
Date: Apr 27, 2005
Subject: Top Flange of Lower Cowl
Any advice on triming off the top flange of the lower cowl for an O-360 engine. I think the same cowl is used on the RV-6, 7 and 8. Cutting off just the flange leaves a rounded edge at the top of the lower cowl. Should I trim off a little more to get a square edge? Thanks for the help Roy Samuelson ________________________________________________________________________________
From: "Jeff Dowling" <shempdowling2(at)earthlink.net>
Subject: Re: Aft Skirts
Date: Apr 27, 2005
I saw it in the 21 years of rv-ator. Jeff ----- Original Message ----- From: "Darrell Reiley" <lifeofreiley2003(at)yahoo.com> Subject: Re: RV-List: Aft Skirts > > And which issue might that be? > > Jeff Dowling wrote:--> RV-List message > posted by: "Jeff Dowling" > > The RV-ator has a trick. It talks about notching your first piece so you > can get an exact fit, then riveting a second thin piece to the first. > > Shemp/Jeff Dowling > RV-6A, N915JD > 190 hours > Chicago/Louisville > ----- Original Message ----- > From: "Pete Howell" > > To: > Subject: RV-List: Aft Skirts > > >> >> Hello, >> >> Anybody have any neat tricks to get the proper curve in the aft slider >> skirts? I have the tops nailed, but the twist along the bottom part is >> vexing. >> >> Cheers, >> >> Pete Howell >> >> >> > > > Darrell Reiley > Round Rock, Texas > RV 7A #70125 > N622DR (reserved) > > --------------------------------- > > > ________________________________________________________________________________
Date: Apr 27, 2005
From: "Tim Bryan" <flyrv6(at)bryantechnology.com>
Subject: Re: Top Flange of Lower Cowl
Roy, I trimmed the upper cowl half first to get it flat and straight. Then put the lower cowl on and the top so the top overlaps the bottom. Marked a line on the bottom using the top as a guide. Cut it there. It was a little more than the given joint in the cowl. Hope that makes sense. Tim RV-6 N616TB -------Original Message------- From: RSamuelson(at)aol.com Date: 04/27/05 07:28:59 Subject: RV-List: Top Flange of Lower Cowl Any advice on triming off the top flange of the lower cowl for an O-360 engine. I think the same cowl is used on the RV-6, 7 and 8. Cutting off just the flange leaves a rounded edge at the top of the lower cowl. Should I trim off a little more to get a square edge? Thanks for the help Roy Samuelson ________________________________________________________________________________
Date: Apr 27, 2005
From: Sam Buchanan <sbuc(at)hiwaay.net>
Subject: Re: Replacement of nav. light lens
bertrv6(at)highstream.net wrote: > > > Hi: > > I have the Aero Flash Nav lights system. After my first flight, the > left side Strobe light, does not work. > > After I checked everything, I called the Mfg. Aero Flash, and they > told me it must be the Power Unit. > > I do not have now any warranty, as have purchased this, more than two > yrs. ago. > > So I have to buy a new power unit...2 questions,1- any other place I > can buy this, at a better price... > > Wonder why only on one side.. > > Finally, when checking, this light, I droped the red lens, that > cover the light. > > Now I see that they want $15.0-0 for 2" red piece of glass.... Any > suggestions on this also, as to where I can get this, for less than > 15.00 plus shipping? plain robbery.... > > > Thanks for your suggestions. > > > Bert Bert, a couple of suggestions based on my experience with this flash system. First, swap power supplies and strobes from side to side (not both at the same time!) to identify for sure whether it is the strobe or power supply that has the problem. I had a strobe to fail very early and upon close inspection, found a component of the strobe bulb inside the potting that was BARELY protruding from the potting and arcing to the grounded shell. This failed the strobe until I insulated the area and then the unit was again operational. Give the failed strobe bulb assembly a very careful inspection to make sure nothing is shorting to ground. I also dropped the red lens (VERY easy to do as you disassemble the unit!). I glued it back together with CA glue temporarily; 5 1/2 years later and I still haven't gotten around to replacing the lens. :-) Sam Buchanan (RV-6, 650 hrs) http://thervjournal.com ________________________________________________________________________________
Date: Apr 27, 2005
From: Bill Dube <bdube(at)al.noaa.gov>
Subject: Re: Replacement of nav. light lens
> > > I have the Aero Flash Nav lights system. After my first flight, >the left side Strobe light, does not work. > > After I checked everything, I called the Mfg. Aero Flash, and they told >me it must be the Power Unit. Have you swapped the left and right strobe connections on the power unit? By swapping the strobe connections on the power unit, you can make sure that the power unit is bad, not the strobe head (or strobe wiring.) > I do not have now any warranty, as have purchased this, more than >two yrs. ago. It may be just urban legend, but I have heard that you should not let a strobe unit sit unused for years on the shelf. Judging from your experience, I guess it would be a good idea to fire up and test your lighting system as soon as it arrives, just to be sure that everything works OK. > So I have to buy a new power unit...2 questions,1- any other place I can >buy this, at a better price... You might be able to get a good deal on a strobe power unit from Bill VonDane at CreativAir <http://www.creativair.com> I know Bill sells complete strobe systems at a very good price, so I suspect he will sell you the power unit alone for a good price as well. I also know that he is very good about customer service and stands behind everything he sells. Bill Dube' ________________________________________________________________________________
From: "Garth Shearing" <Garth(at)islandnet.com>
Subject: Re: Flluroescent Light Tach Calibration
Date: Apr 27, 2005
I calibrated my two-bladed prop at night with the prop near the hangar door where the ceiling flourescent lights were. If you are calibrating, use 1200 or 1800, whatever works. You can easily see the stroboscopic effect as you go through various RPM's. Don't use a battery-operated flourescent light for obvious reasons. Cheers. Garth Shearing VariEze & 90% RV6A Victoria BC Canada > > I know that I've read someplace that you can calibrate a tach using a 60hz > fluorescent light. Can anyone give me the two blade rpms that will stop > the prop? I need to calibrate a tach. > > Thanks > > Mike Holland ________________________________________________________________________________
From: "Becki" <becki@fly-gbi.com>
Subject: Construction Videos available in DVD format
Date: Apr 27, 2005
Just wanted to let everyone know that we are now offering our construction videos in DVD format. The prices are the same as for the VHS versions. Please give us a call (940) 648-0841 or email us if we can help you with these. Thanks to everyone for their patience and support! Becki Orndorff GeoBeck, Inc. www.fly-gbi.com 940-648-0841 ________________________________________________________________________________
Date: Apr 27, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: Aft Skirts
Thanks my friend! Jeff Dowling wrote: I saw it in the 21 years of rv-ator. Jeff ----- Original Message ----- From: "Darrell Reiley" Subject: Re: RV-List: Aft Skirts > > And which issue might that be? > > Jeff Dowling wrote:--> RV-List message > posted by: "Jeff Dowling" > > The RV-ator has a trick. It talks about notching your first piece so you > can get an exact fit, then riveting a second thin piece to the first. > > Shemp/Jeff Dowling > RV-6A, N915JD > 190 hours > Chicago/Louisville > ----- Original Message ----- > From: "Pete Howell" > > To: > Subject: RV-List: Aft Skirts > > >> >> Hello, >> >> Anybody have any neat tricks to get the proper curve in the aft slider >> skirts? I have the tops nailed, but the twist along the bottom part is >> vexing. >> >> Cheers, >> >> Pete Howell >> >> >> > > > Darrell Reiley > Round Rock, Texas > RV 7A #70125 > N622DR (reserved) > > --------------------------------- > > > Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) --------------------------------- ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Fuel Purge Line Question
Date: Apr 27, 2005
According to my memory of a conversation with Airflow Performance maybe a year ago, the purge line serves two purposes. The primary reason is to circulate hot fuel out of the system and back into the lines between the tanks and the fuel pump to make hot starts easier. I have mine returning to the right fuel tank line before the fuel valve. If I start with the fuel valve set to feed from the left tank, the presumably hot fuel returns to the right tank as the fuel pump pumps from the left tank. I was also told that even if I started from the right tank, just running the hot fuel back through the lines and the fuel pump would probably be sufficient cooling to get things going. The other reason for the purge valve is to shut down the engine. Apparently the mixture doesn't reliably stop enough fuel going to the engine to stop it. Lots of stuff on this in the archives. Terry RV-8A finishing Seattle ________________________________________________________________________________
Date: Apr 27, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: AFS (Aircraft Finishing Systems) stuff for corrosion protection
I'm doing a QB RV-7A but still need to decide on a corrosion protected mechanism for the tail. I am really interestd in the AFS stuff for its non-toxic qualities. A search of the archive provided few hits re: priming/corrosion protection with this stuff. Has anybody used the AFS stuff or know somebody that did? Did you use all three of the products - cleaner, etch, primer? Is it possible to apply the primer by dipping parts in a tub or does it need to be sprayed HVLP? ________________________________________________________________________________
Date: Apr 27, 2005
From: Richard Tasker <retasker(at)optonline.net>
Subject: Re: AFS (Aircraft Finishing Systems) stuff for corrosion
protection I have used the aluminum cleaner/etch and the primer. Both worked fine as far as ease of use and ease of application. The primer seems very rugged - you can dimple aluminum with the primer applied and it stays put. I can't say how well it works over time since I am still building. I am sure you could dip parts if you wanted, but it would be a bit expensive. It can be sprayed with any sprayer (not just HVLP) or can be painted on to small pieces. Dick Tasker Paul Folbrecht wrote: > >I'm doing a QB RV-7A but still need to decide on a corrosion protected >mechanism for the tail. > >I am really interestd in the AFS stuff for its non-toxic qualities. A search >of the archive provided few hits re: priming/corrosion protection with this >stuff. > >Has anybody used the AFS stuff or know somebody that did? Did you use all >three of the products - cleaner, etch, primer? Is it possible to apply the >primer by dipping parts in a tub or does it need to be sprayed HVLP? > > > > ________________________________________________________________________________
Subject: QB Fuse Work
From: "" <tx_jayhawk(at)excite.com>
Date: Apr 27, 2005
All, I have my SB wings and tail completed, and I am expecting my QB fuse in June. I have been debating about whether or not it makes sense to go ahead and order the finishing kit as well to ship with the fuse. Can anyone comment on the amount of work left on the QB fuse (assuming you have no engine, avionics, or finishing kit)? Will I find that I need the finishing kit (or other items) very quickly? What would be the preferred order of purchase (finish, engine, or panel stuff). I am planning avionics last, as it changes so quickly. Thanks,Scott7A ________________________________________________________________________________
Date: Apr 27, 2005
From: Bobby Hester <bhester(at)hopkinsville.net>
Subject: Re: QB Fuse Work
tx_jayhawk(at)excite.com wrote: > > All, I have my SB wings and tail completed, and I am expecting my QB fuse in June. I have been debating about whether or not it makes sense to go ahead and order the finishing kit as well to ship with the fuse. Can anyone comment on the amount of work left on the QB fuse (assuming you have no engine, avionics, or finishing kit)? Will I find that I need the finishing kit (or other items) very quickly? What would be the preferred order of purchase (finish, engine, or panel stuff). I am planning avionics last, as it changes so quickly. Thanks,Scott7A > > > Finish kit then panel stuff and the engine last. Best not to have the engine just sitting around for a long time. Also keep in mind that you need warm weather when your doing the canopy work or at least a warm place to do it, I did mine in the hanger so I had to plan it for the warm weather. I did most of it last summer and will be finishing it up sometime over the next couple months. -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse :-) ________________________________________________________________________________
Date: Apr 27, 2005
From: Dave Bristol <dbris200(at)sbcglobal.net>
Subject: Re: Fuel Purge Line Question
I chose to tee into the line from the right tank to the valve because I almost always take off on the left tank. I do this because the airplane (- 6) is out of balance laterally with just me and full fuel, so burning the left tank first tends to balance the load quicker. Doing it this way means that the purged fuel is going to the un-selected tank. I originally tee'd into the vent line but had to change it because it tended to pump fuel out on the ground, probably because it was pumping into a smaller line and the fuel went both directions in the vent line. Just be sure that the totalizer is turned off when you start and you won't have any errors due to the purged fuel - although, the amount of fuel that is purged shouldn't even be noticeable in the total fuel burn so I wouldn't worry about it. Dave -6 So Cal EAA Technical Counselor Dwight Frye wrote: > >I have seen a number of approaches to handling the fuel return >for the purge line in fuel injected setups. I have seen things >arranged such that the line T's into the supply line of one tank >(the one not currently being used, say, the left). I have also >seen things arranged so that the fuel purges back all the way into >the tank which is selected. > > > > ________________________________________________________________________________
From: "Greg Young" <gyoung@cs-sol.com>
Date: Apr 28, 2005
Subject: Re: Fuel Purge Line Question
I definitely would NOT tee the purge line into the vent line. I tee'd it to the vent line on my first but will route it to the tank on the Phoenix. There is a lot of discussion on it in the archives on approaches and the possible failure modes. The concensus safest approach was to return the purge to the tank near the bottom so that the line would always be immersed in fuel. This is to preclude the possibility of injesting air if the purge valve leaks or works open in flight. Remember the vent line is slightly pressurized in flight. It might be a low probability event but the consequence could ruin your day. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A Dwight, I am using an Airflow Performance injection system. I simply routed the line from the purge valve to a 'T' into the vent line on my right tank. If you put the 'T' at the low (tank) side of the vertical loop of the vent line, the pump will send fuel into the tank through the vent with the valve on the "purge" setting. The vertical loop in the vent line will keep the fuel from being pumped onto the ground. With the purge valve at the "run" setting the tank will vent normally. If your tanks are full, your fuel selector must be set on the tank the purge valve will send the fuel to (in my case the right tank) or you will overflow the opposite tank. This will create a closed loop with cool fuel being sucked from the tank while the hot fuel is pumped in through the vent. If your tanks aren't full it doesn't make any difference. It will just pump fuel from one tank to the other. This has worked fine for me, but I have yet to do any hot starts in temperatures above 80 degrees. E-mail me off line if you'd like pictures. Ted RV-4 ________________________________________________________________________________
From: "Ed Holyoke" <bicyclop(at)pacbell.net>
Subject: Re: Fuel Purge Line Question
Date: Apr 27, 2005
How about a check valve just before the tee to prevent any air ingestion via the purge? Ed Holyoke -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Greg Young Subject: RV-List: Re: Fuel Purge Line Question I definitely would NOT tee the purge line into the vent line. I tee'd it to the vent line on my first but will route it to the tank on the Phoenix. There is a lot of discussion on it in the archives on approaches and the possible failure modes. The concensus safest approach was to return the purge to the tank near the bottom so that the line would always be immersed in fuel. This is to preclude the possibility of injesting air if the purge valve leaks or works open in flight. Remember the vent line is slightly pressurized in flight. It might be a low probability event but the consequence could ruin your day. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A > Dwight, I am using an Airflow Performance injection system. I simply routed the line from the purge valve to a 'T' into the vent line on my right tank. If you put the 'T' at the low (tank) side of the vertical loop of the vent line, the pump will send fuel into the tank through the vent with the valve on the "purge" setting. The vertical loop in the vent line will keep the fuel from being pumped onto the ground. With the purge valve at the "run" setting the tank will vent normally. If your tanks are full, your fuel selector must be set on the tank the purge valve will send the fuel to (in my case the right tank) or you will overflow the opposite tank. This will create a closed loop with cool fuel being sucked from the tank while the hot fuel is pumped in through the vent. If your tanks aren't full it doesn't make any difference. It will just pump fuel from one tank to the other. This has worked fine for me, but I have yet to do any hot starts in temperatures above 80 degrees. E-mail me off line if you'd like pictures. Ted RV-4 ________________________________________________________________________________
From: "Ross S" <rv7maker(at)hotmail.com>
Subject: RV-7 for Sale!
Date: Apr 27, 2005
Ladies and Gents, If you know of anyone interesed in a 7, have them check out: http://www.experimentalair.com/n703rv/forsale.html Thanks, Ross Ross Schlotthauer Experimental Air ________________________________________________________________________________
Date: Apr 28, 2005
From: Doug Gray <dgra1233(at)bigpond.net.au>
Subject: Re:Advice on using an off-set rivet set
Hmmmm.... I use as a starting point approx 25psi for 3/32, 40psi for 1/8 and I noted when doing my '6 mainspars I used 75psi for the 3/16" rivets. Pressures are at the compressor. No difficulty setting the large rivets with a gun but I did need eardefenders; and before I was done my neightbours kids had begun throwing rocks (small ones) at me. It was a tad noisy. For the record I wouldn't dream of using an offset set for the 3/16" rivets. It's just too much energy to keep under control. Doug Gray Bob Hodgson wrote: > > Mike, > Offset rivet sets do try to rotate unless you duct tape them to the gun at > around 45 deg, and/or restrain them with your other hand. Unless you're > over-endowed with hands, this may mean an assistant on the bucking bar! > > Is this an AN470AD6-x or an AN470AD4-6 ? If it's a 3/16 diameter rivet, you > need a lot of pressure and at least a 4X gun, so it will need a VERY firm > grip to control it. Try leaning on it as you squeeze the trigger, and get > your assistant to allow the bar to bounce a little on the shop head rather > than hold it immovably against it. > > FWIW, I use 35 psi for 3/32 and 45 for 1/8 (measured at the compressor). > Haven't had to do any 3/16, but would try 55 for a start, or buy a big > squeezer. > > Good Luck, > Bob (UK) > RV3B (still 'finishing' . . ) > > ----- Original Message ----- > > >>From: MLWynn(at)aol.com >>Subject: RV-List: >> >> >>Hi folks >> >>I have a single universal head -6 rivet to set. An offset set gives me a >>much better angle to get to it. However, when I tried to use the thing in > > my > >>practice piece, it rotated and jumped and was generally nearly impossible > > to > >>control. Is there a trick to this? >> >>Regards, >> >>Michael Wynn >>RV-8, Empennage >>San Ramon, California > > > > > > > > ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: Apr 28, 2005
Subject: Re: Flluroescent Light Tach Calibration
In a message dated 4/26/05 11:06:04 PM Central Daylight Time, retasker(at)optonline.net writes: > Can anyone give me the two blade rpms that will stop the prop? I need to > calibrate a tach. > >>>> From the Grand Rapids EIS4000 User's Manual, Section 6.2: (for 60Hz) 2-blade prop: 600 720 1200 1440 1800 3600 3-blade prop: 240 300 480 600 1200 2400 Their procedure states: "A simple test to help verify the RPM readings are accurate can be made by running the engine at night, and looking through the propeller at a flourescent or mercury vapor light. The pulsation of the light will make the propeller to appear to (be) stopped at various RPMs." Mark ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: QB Fuse Work
Date: Apr 28, 2005
Scott, We ordered our finish kit with our QB fuse together and were glad we did. It help the work flow much smoother. Good Building, Chuck Rowbotham RV-8A >From: "" <tx_jayhawk(at)excite.com> >Reply-To: rv-list(at)matronics.com >To: rv-list(at)matronics.com >Subject: RV-List: QB Fuse Work >Date: Wed, 27 Apr 2005 21:01:46 -0400 (EDT) > > > All, I have my SB wings and tail completed, and I am expecting my QB fuse >in June. I have been debating about whether or not it makes sense to go >ahead and order the finishing kit as well to ship with the fuse. Can >anyone comment on the amount of work left on the QB fuse (assuming you have >no engine, avionics, or finishing kit)? Will I find that I need the >finishing kit (or other items) very quickly? What would be the preferred >order of purchase (finish, engine, or panel stuff). I am planning avionics >last, as it changes so quickly. Thanks,Scott7A > > ________________________________________________________________________________
From: RSamuelson(at)aol.com
Date: Apr 28, 2005
Subject: Trimming lower cowl top flange
I'll answer my own question to get it in the archieves. Don't trim the top of the cowl beyond the flange at least not until it is fitted everywhere else. As received from Van's, mine had very little overlap between the upper and lower cowl. Had I trimmed another quarter inch they might not join together. I'll try to mix up some epoxy microballons (or something) to fill in this small area. Roy Samuelson ________________________________________________________________________________
From: <kbob(at)cox.net>
Subject: Top Flange of Lower Cowl
Date: Apr 28, 2005
Hi Roy, I am at this exact point in mounting my cowl and will share my experience on the O-320-6A pre-preg cowl... The top cowl was not cut at all along the horizontal seams, just edge sanded & fit at the firewall. Then to the lower cowl: I cut the flange on the seam right to the line. It is a little rough in spots with air bubbles, pinholes & rounding. When the lower cowl was finally trimmed & fit this seam needed almost no more trimming. Only spot sanding to get the seam tight. I will need to fill the edge bubbles and pinholes to make it nice. Any further trimming would have been too much. It is slightly rounded in spots. You really need to take this cowl on and off at least a dozen times and trim 1/16" here and there until it is good. It is good practice for the future when you will be removing it for maintenance. And it will make you happy you didn't build a plastic plane ;-) Kelly Patterson PHX, AZ N716K RV-6A FWF From: RSamuelson(at)aol.com Subject: RV-List: Top Flange of Lower Cowl Any advice on triming off the top flange of the lower cowl for an O-360 engine. I think the same cowl is used on the RV-6, 7 and 8. Cutting off just the flange leaves a rounded edge at the top of the lower cowl. Should I trim off a little more to get a square edge? Thanks for the help Roy Samuelson ________________________________________________________________________________
Date: Apr 28, 2005
From: Ted Lumpkin <tlump51(at)sbcglobal.net>
Subject: Re: Fuel Purge Line Question
Greg, Good points. Regarding failure modes, in my view if the purge valve works open in flight the engine is going to quit regardless of where your return line is plumbed (at least with the Airflow Performance system). Although the vent line is slightly pressurized in flight, it's pressure is much lower than the 20 - 40 psi that the fuel system is running at. It's very unlikely that air from the vent line would be "sucked" into a pressurized system. I believe Mike Stewart mentioned that he had a problem with a cracked purge return line allowing air into the system, but I believe his purge line was routed back to the fuel supply line, not the vent. Ted Greg Young <gyoung@cs-sol.com> wrote: I definitely would NOT tee the purge line into the vent line. I tee'd it to the vent line on my first but will route it to the tank on the Phoenix. There is a lot of discussion on it in the archives on approaches and the possible failure modes. The concensus safest approach was to return the purge to the tank near the bottom so that the line would always be immersed in fuel. This is to preclude the possibility of injesting air if the purge valve leaks or works open in flight. Remember the vent line is slightly pressurized in flight. It might be a low probability event but the consequence could ruin your day. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A Dwight, I am using an Airflow Performance injection system. I simply routed the line from the purge valve to a 'T' into the vent line on my right tank. If you put the 'T' at the low (tank) side of the vertical loop of the vent line, the pump will send fuel into the tank through the vent with the valve on the "purge" setting. The vertical loop in the vent line will keep the fuel from being pumped onto the ground. With the purge valve at the "run" setting the tank will vent normally. If your tanks are full, your fuel selector must be set on the tank the purge valve will send the fuel to (in my case the right tank) or you will overflow the opposite tank. This will create a closed loop with cool fuel being sucked from the tank while the hot fuel is pumped in through the vent. If your tanks aren't full it doesn't make any difference. It will just pump fuel from one tank to the other. This has worked fine for me, but I have yet to do any hot starts in temperatures above 80 degrees. E-mail me off line if you'd like pictures. Ted RV-4 ________________________________________________________________________________
Date: Apr 28, 2005
From: Bob <panamared3(at)brier.net>
Subject: Re: Fuel Purge Line Question
clamav-milter version 0.80j on opie.wvnet.edu Just last night I was talking to Don Rivera of Airflow performance about the purge system. If you use his system he gives you a plumbing diagram, which states to run the purge line to a T in the right tank feed line before the fuel selector and or fuel filter. Use left tank for purging and shutdown. As for fuel totalizer. The amount of fuel during a purge is very small, measured in ounces. He told me that the during the purge process you will be moving fuel at about 3 to 4 GPH. 3 GPH is about 6 oz per minute. Also Don recommends flexible hose from purge valve to firewall and then aluminum tubing inside cockpit. Cheaper and lighter than flex all the way, and aluminum tube in front of firewall is subject to cracking. If you use a gascolator, call Don. He did ask me if I used one, when I told him I didn't we dropped the subject. I think there is more to the story! For more what ifs and best practices call Don. He is a great guy to talk to and he really knows all the answers. For those who are true experimenters, experiment away and let us know the results. If you only want to do it once and have confidence that it will work right the first time, follow manufactures instructions. Bob RV6 NightFighter ________________________________________________________________________________
Date: Apr 28, 2005
From: Darrell Reiley <lifeofreiley2003(at)YAHOO.COM>
Subject: Re: QB Fuse Work
Scott, If the cash is not an issue, just the savings in freight will benefit you shipping them together. And yes... you will want to start playing with the canopy. Call Jeff and get his opinion... Darrell wrote: All, I have my SB wings and tail completed, and I am expecting my QB fuse in June. I have been debating about whether or not it makes sense to go ahead and order the finishing kit as well to ship with the fuse. Can anyone comment on the amount of work left on the QB fuse (assuming you have no engine, avionics, or finishing kit)? Will I find that I need the finishing kit (or other items) very quickly? What would be the preferred order of purchase (finish, engine, or panel stuff). I am planning avionics last, as it changes so quickly. Thanks,Scott7A Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) ________________________________________________________________________________
From: "Brad Oliver" <brad(at)rv7factory.com>
Subject: Belt Sander Question & Tool Resource
Date: Apr 28, 2005
I've been lurking here for a few months, but now I have a question, and a resource that might help others. I am in the tooling up phase, and I have a question about belt sanders. At one of the last EAA chapter events I attended, a few people said a belt sander was a highly useful tool, one member actually said he wish he had bought his sooner. I took this as a recommendation to buy one. My question is, in purchasing a belt sander, are their particular features I should look for or stay away from? Craftsman has a 2x42" belt / 6" disc unit that looks nice... will it do the job? Ok, now for the resource I found... In my tool research (grinders, drill presses, band saws, etc.) I came across this site: http://www.rd.com/americanwoodworker/article.do?siteId=2222&categoryId=7002& contentId=244 They have reviews and specs for very many of the available tools made today. The spec charts are very useful to compare tools, with speeds, capacities, and prices all listed. It has helped me tremendously and maybe it can help others. Regards, Brad Oliver Livermore, CA Tooling up... RV-7 Very Soon! ________________________________________________________________________________
From: Dwight Frye <dwight(at)openweave.org>
Subject: Re: Fuel Purge Line Question
Date: Apr 28, 2005
Bob, Thanks for passing on the info from AFP. I will, in fact, be using an AFP FI system. There are things I do want to experiement with ... but the fuel system isn't one of them. :) I think I'll just take AFP's advice here. -- Dwight On Thu Apr 28 14:19:27 2005, Bob wrote : > > >Just last night I was talking to Don Rivera of Airflow performance about >the purge system. If you use his system he gives you a plumbing diagram, >which states to run the purge line to a T in the right tank feed line >before the fuel selector and or fuel filter. Use left tank for purging and >shutdown. > >As for fuel totalizer. The amount of fuel during a purge is very small, >measured in ounces. He told me that the during the purge process you will >be moving fuel at about 3 to 4 GPH. 3 GPH is about 6 oz per minute. > >Also Don recommends flexible hose from purge valve to firewall and then >aluminum tubing inside cockpit. Cheaper and lighter than flex all the way, >and aluminum tube in front of firewall is subject to cracking. > >If you use a gascolator, call Don. He did ask me if I used one, when I >told him I didn't we dropped the subject. I think there is more to the story! > >For more what ifs and best practices call Don. He is a great guy to talk >to and he really knows all the answers. > >For those who are true experimenters, experiment away and let us know the >results. If you only want to do it once and have confidence that it will >work right the first time, follow manufactures instructions. > >Bob >RV6 NightFighter ________________________________________________________________________________
From: "Charles Heathco" <cheathco(at)comcast.net>
Subject: Oily soot in lft tailpipe
Date: Apr 28, 2005
I noticed this on antenna which is sorta behind left pipe after last flight, and today being first really nice flying day in a while, I took "tweety bird' (6a with stock O-320) for a spin. Not as much but some soot on ant, and inside of left pipe was very sooty, rt pipe clean as a whistle. Im getting good static and power seems normal. Altho I cant see a relationship, i just installed OH'd mags, and very recent OH'd carb. Cyls all tested in the mid high 70's about 40 hrs ago. Also since I had dynamic prop balance I cant run wide open without going over prop redline. Oil usage is and has been normal, about 11-12hrs qt. Again, she seems to be running like a top, but what should I be looking ofr with this oily soot in the lft pipe? charlie heathco ________________________________________________________________________________
Date: Apr 28, 2005
From: Walter Tondu <walter(at)tondu.com>
Subject: Re: Belt Sander Question & Tool Resource
On 04/28 12:58, Brad Oliver wrote: > > I've been lurking here for a few months, but now I have a question, and a > resource that might help others. > > I am in the tooling up phase, and I have a question about belt sanders. At > one of the last EAA chapter events I attended, a few people said a belt > sander was a highly useful tool, one member actually said he wish he had > bought his sooner. I took this as a recommendation to buy one. My question > is, in purchasing a belt sander, are their particular features I should look > for or stay away from? Craftsman has a 2x42" belt / 6" disc unit that looks > nice... will it do the job? I think you mean "bench" sander. I actually couldn't think of any uses for a belt sander off hand. Harbor Freight has some nice bench sanders for minimal cost. This is the one I have and it kicks ass. I used it every day during my build. http://www.harborfreight.com/cpi/ctaf/Displayitem.taf?itemnumber=43468 -- Walter Tondu http://www.rv7-a.com ________________________________________________________________________________
Date: Apr 28, 2005
From: linn walters <lwalters2(at)cfl.rr.com>
Subject: Re: Oily soot in lft tailpipe
Charles Heathco wrote: > >I noticed this on antenna which is sorta behind left pipe after last flight, and today being first really nice flying day in a while, I took "tweety bird' (6a with stock O-320) for a spin. Not as much but some soot on ant, and inside of left pipe was very sooty, rt pipe clean as a whistle. Im getting good static and power seems normal. Altho I cant see a relationship, i just installed OH'd mags, and very recent OH'd carb. Cyls all tested in the mid high 70's about 40 hrs ago. Also since I had dynamic prop balance I cant run wide open without going over prop redline. Oil usage is and has been normal, about 11-12hrs qt. Again, she seems to be running like a top, but what should I be looking ofr with this oily soot in the lft pipe? charlie heathco > You've just discovered on of the down sides to having a carbureted engine. They just don't get the same amount of fuel to the cylinders as a FI system. So, you lean until it stumbles and richen it up a bit ......but you only got one (or maybe two) cylinders lean enough to run well. The others are running rich. There is something you can check though. Intake leaks. You'd be amazed at how many engines are out there with leaky intake systems. Take a shop vac (clean it out real good!) that you can switch the hose to exhaust and put the output into your air intake. Seal it with some rags and spray soapy water everywhere. Look for bubbles. The other thought I had was that you may have a carb gasket that isn't sealing ....... and you'll see the bubbles! The gasket that goes between the carb body and the top may not be sealing well either, allowing raw fuel to enter the vinturi directly from the float bowl. This will unbalance the fuel delivery a lot, causing just what your symptoms are. Sometimes that gasket will swell a little and seal off the leak. Since you had the carb OH'd recently, I'd suspect something with the carb too. Just a quick shot in the dark!!! Best of luck .... and let us know what you find! Linn > > > > -- ________________________________________________________________________________
Date: Apr 28, 2005
From: "John D. Heath" <Alto_Q(at)direcway.com>
Subject: Re: Oily soot in lft tailpipe
Charlie, I would check the plugs on those two cylanders. If you find an oily one look at the rocker box drain tube and valve guides. Even if you don't find an oily plug, a worn exhaust valve guide can still pass oil and bypass the combustion chamber. John D. Heath ----- Original Message ----- From: "Charles Heathco" <cheathco(at)comcast.net> Subject: RV-List: Oily soot in lft tailpipe > > I noticed this on antenna which is sorta behind left pipe. Again, she > seems to be running like a top, but what should I be looking ofr with this > oily soot in the lft pipe? charlie heathco > > > ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Control sticks with bend/left-hand throttle quadrant
Two unrelated questions: 1) I know I have seen RVs with control sticks with a forward bend in them. I want them cause they look much cooler than the straight sticks. Who makes them? 2) It seems it's pretty customary to put the engine controls on the panel, meaning used with right hand, which I assume means stick in left hand. Of course I fly yoke-equipped planes with my left on the yoke but I think that using my right hand on a control stick might be far more natural (I am right-handed, like all good Americans*). The only time I have in stick-controlled aircraft is my RV-10 demo ride and a couple flights in a Challenger UL, and in both cases I used my right on the stick. With those thoughts, I was thinking that a left-hand engine-control arrangement might really be ideal. Thoughts on this?? Does anyone make an aftermarket side-mounted throttle-quadrant. Should I just learn to fly with my left hand on the stick like everybody else? * Just kidding. ________________________________________________________________________________
Date: Apr 28, 2005
From: rv6fly <rv6fly(at)bresnan.net>
Subject: Re: Belt Sander Question & Tool Resource
Brad Oliver wrote: >I am in the tooling up phase, and I have a question about belt sanders. At >one of the last EAA chapter events I attended, a few people said a belt >sander was a highly useful tool, one member actually said he wish he had >bought his sooner. > Brad, I think a hand-held belt sander is a great tool. I used a "Sandcat" by skill (2 1/2x 16 inch belt, I believe, and no longer made) on a Glasair, RV6, Glastar and my friend's 6A project. It gave up the ghost on the 6A. Got so hot I couldn't hold on to it. I think it ingested too much fiberglass dust. I'm going to tear it apart and see if there is anything that I can do to fix it and take it over to Larry in Spearfish so he can use it on his cowl. With various grits of paper, it's a very versitle tool and does a great job of replacing a file. For removing material quickly down to a line, whether aluminum or fiberglass, it can't be beat. Start with coarse grit and change to fine as you get close to the line. I used the fine grit and touched up all edges of both sheet stock and ribs & bulkheads before using the double edge deburring tool which eleminates "chatter" marks and results in a quicker and smoother job. The hand held models were preferable to me because of portabililty. Buy the lightest one you can find. Some of the bigger ones would get heavy after not too much use I'd think. Bob Skinner Buffalo, WY -- ________________________________________________________________________________
Date: Apr 28, 2005
From: Ron Lee <ronlee(at)pcisys.net> quadrant
Subject: Re: Control sticks with bend/left-hand throttle
quadrant >Of >course I fly yoke-equipped planes with my left on the yoke but I think that >using my right hand on a control stick might be far more natural (I am >right-handed, like all good Americans*). I am right handed and fly the RV-6A with my left hand with NO problem. Actually I think flying with my right hand would be odd. Ron Lee ________________________________________________________________________________
Date: Apr 28, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
On 15:26:38 2005-04-28 Paul Folbrecht wrote: > With those thoughts, I was thinking that a left-hand engine-control > arrangement might really be ideal. Thoughts on this?? Does anyone > make an aftermarket side-mounted throttle-quadrant. Should I just > learn to fly with my left hand on the stick like everybody else? All the flying I can remember doing before starting my pilot's license was in the passenger seat of an airplane, which meant either right hand on a yoke, left hand on throttle, or right hand on stick, left hand on throttle. When I learned to fly, I was thrown into the left seat of a C-150, and had absolutely no trouble flying left hand on yoke, right on throttle. After getting my license, my only two choices were left seat in a C-150 (yoke), or centerline seat in the club homebuilt (stick). No problems moving back and forth. Last year I was introduced to left hand stick, right hand throttle on a formation flight in an RV. I flew for an hour, and for the life of me couldn't get my hands to switch jobs. My brain seems locked into my left hand controlling pitch if i'm holding a stick with either hand. I eventually managed to get myself to pause before any corrective inputs, and think first what I wanted to do. So, my RV-7 will be flown from the right seat, with a single, center console mounted throttle. I already have the throttle, and know where it will go (in front of the spar, between the seats, pending relocation of the fuel selector). That way it will be accessible to both pilots, but I can fly how i'm comfortable. -Rob ________________________________________________________________________________
From: "son hoang" <son(at)hoangs.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
easy solution fly from the right seat all CFI do it daily ----- Original Message ----- From: "Paul Folbrecht" <paulfolbrecht(at)yahoo.com> Subject: RV-List: Control sticks with bend/left-hand throttle quadrant > > Two unrelated questions: > > 1) I know I have seen RVs with control sticks with a forward bend in them. I > want them cause they look much cooler than the straight sticks. Who makes > them? > > 2) It seems it's pretty customary to put the engine controls on the panel, > meaning used with right hand, which I assume means stick in left hand. Of > course I fly yoke-equipped planes with my left on the yoke but I think that > using my right hand on a control stick might be far more natural (I am > right-handed, like all good Americans*). The only time I have in > stick-controlled aircraft is my RV-10 demo ride and a couple flights in a > Challenger UL, and in both cases I used my right on the stick. > > With those thoughts, I was thinking that a left-hand engine-control arrangement > might really be ideal. Thoughts on this?? Does anyone make an aftermarket > side-mounted throttle-quadrant. Should I just learn to fly with my left hand > on the stick like everybody else? > > * Just kidding. > > ________________________________________________________________________________
From: "Bill Schlatterer" <billschlatterer(at)sbcglobal.net>
Subject: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
OK Stick right and throttle on left but where is everything else? If side by side, 6, 7, 10, IFR or not, Which hand do you write with, which hand would you normally work the radios and nav/coms, where is the AP, which hand switches fuel tanks, which hand would you likely be drinking coffee with ;o) Just something to think about? Bill S 7a Ark -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Paul Folbrecht Subject: RV-List: Control sticks with bend/left-hand throttle quadrant Two unrelated questions: 1) I know I have seen RVs with control sticks with a forward bend in them. I want them cause they look much cooler than the straight sticks. Who makes them? 2) It seems it's pretty customary to put the engine controls on the panel, meaning used with right hand, which I assume means stick in left hand. Of course I fly yoke-equipped planes with my left on the yoke but I think that using my right hand on a control stick might be far more natural (I am right-handed, like all good Americans*). The only time I have in stick-controlled aircraft is my RV-10 demo ride and a couple flights in a Challenger UL, and in both cases I used my right on the stick. With those thoughts, I was thinking that a left-hand engine-control arrangement might really be ideal. Thoughts on this?? Does anyone make an aftermarket side-mounted throttle-quadrant. Should I just learn to fly with my left hand on the stick like everybody else? * Just kidding. ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
Tracy Saylor used to (and maybe still does) sell a left hand throttle quadrant for the RV-6. I have one in my airplane and really like it. If Tracy no longer sells the unit, contact me off-list and I'll sketch it so you can fabricate one yourself. My guess is that it would take under 5 hours... KB ----- Original Message ----- From: "Paul Folbrecht" <paulfolbrecht(at)yahoo.com> Subject: RV-List: Control sticks with bend/left-hand throttle quadrant > > Two unrelated questions: > > 1) I know I have seen RVs with control sticks with a forward bend in them. > I > want them cause they look much cooler than the straight sticks. Who makes > them? > > 2) It seems it's pretty customary to put the engine controls on the panel, > meaning used with right hand, which I assume means stick in left hand. Of > course I fly yoke-equipped planes with my left on the yoke but I think > that > using my right hand on a control stick might be far more natural (I am > right-handed, like all good Americans*). The only time I have in > stick-controlled aircraft is my RV-10 demo ride and a couple flights in a > Challenger UL, and in both cases I used my right on the stick. > > With those thoughts, I was thinking that a left-hand engine-control > arrangement > might really be ideal. Thoughts on this?? Does anyone make an > aftermarket > side-mounted throttle-quadrant. Should I just learn to fly with my left > hand > on the stick like everybody else? > > * Just kidding. > > > ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
No trouble initially, either? It didn't take getting used to? It is funny that flying a yoke with my left is completely natural yet I know (or think I know) that a stick in my left and will not feel that way. Maybe that's just because my very, very limited "_stick_ time" has been with my right. If that's the case, I should be used to the left in < 2 hours. > I am right handed and fly the RV-6A with my left hand with NO problem. > Actually I think flying with my right hand would be odd. ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
Have you flown right-seat before? The sight picture on landing is quite different - it takes getting used to! You can't just jump into landing that way. At least I couldn't. > So, my RV-7 will be flown from the right seat, with a single, center > console mounted throttle. I already have the throttle, and know where it > will go (in front of the spar, between the seats, pending relocation of the > fuel selector). That way it will be accessible to both pilots, but I can > fly how i'm comfortable. > > -Rob > > > > > > > > ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
They trained to do it too. --- son hoang wrote: > > easy solution > fly from the right seat > all CFI do it daily ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Control sticks with bend/left-hand throttle quadrant
1) IFR, the AP is on. :-) 2) I've gotta write with the right hand. I can do better with a foot than with the left. 3) Right now I do everything with the right hand except fly (yoke). The cockpit/panel is designed for that anyway when you're in the left seat. Of course. I see your point. If I've got my RH on the stick I've got no hand to do all that other stuff. Ain't gonna work at all. I'm sure I can get used to the left. > OK Stick right and throttle on left but where is everything else? If side > by side, 6, 7, 10, IFR or not, Which hand do you write with, which hand > would you normally work the radios and nav/coms, where is the AP, which hand > switches fuel tanks, which hand would you likely be drinking coffee with ;o) > Just something to think about? > > Bill S > 7a Ark ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
> >1) I know I have seen RVs with control sticks with a forward bend in them. Nobody answered this part - does anybody know? Those sticks seriously looked so good and the bend is quite functional as well! Perhaps they were custom jobs. ________________________________________________________________________________
From: "son hoang" <son(at)hoangs.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
don't worry...you'll get used to it in no time at all ----- Original Message ----- From: "Paul Folbrecht" <paulfolbrecht(at)yahoo.com> Subject: Re: RV-List: Control sticks with bend/left-hand throttle quadrant > > Have you flown right-seat before? The sight picture on landing is quite > different - it takes getting used to! You can't just jump into landing that > way. At least I couldn't. > > > So, my RV-7 will be flown from the right seat, with a single, center > > console mounted throttle. I already have the throttle, and know where it > > will go (in front of the spar, between the seats, pending relocation of the > > fuel selector). That way it will be accessible to both pilots, but I can > > fly how i'm comfortable. > > > > -Rob > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "LARRY ADAMSON" <rvhi03(at)msn.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
----- Original Message ----- From: Paul Folbrecht Subject: RV-List: Control sticks with bend/left-hand throttle quadrant I'm technically left handed, but do precision metal snipping, shooting, bowling, throwing, and more with my right. Eat, write, and drink coffee with my left. Flew the Pitt's, R/C airplanes, and computer joysticks with my right, as it seems the natural way. First time I flew a Cessna from the right seat, I pulled throttle out instead of rotating during a second touch and go. Even a Cessna 172 likes to bee-line to the right when engine goes to idle just at rotation time! That was just a case of thinking "left hand & plane with yoke rotation", but I soon learned different! I naturally wondered how I'd feel in the RV too. Rented a Diamond DA-40 just to get some left hand stick time, along with differential brakes for taxi. As it turned out, I didn't even think about it. My left hand seemed as natural on the stick as it does with a yoke. But since this subject has come up, while sitting in my (almost completed) RV6A's left seat, my left hand still feels the most comfortable on the stick while my elbow is on the arm rest. I've also flown the 6 & 9 from the right seat, where again, the right hand now seems to fit the best. In so many words, it doesn't seem to matter , right or left. I went out to the 6A again this evening. If I could put in an ill fitted and tight throttle quadrant on the left (which is possible and has been done), I wouldn't. It just no longer feels right, as strange as it may be. Larry Adamson ________________________________________________________________________________
Date: Apr 28, 2005
From: Ron Lee <ronlee(at)pcisys.net> quadrant
Subject: Re: Control sticks with bend/left-hand throttle
quadrant >No trouble initially, either? It didn't take getting used to? I also flew Cessnas with left hand on the yoke so the transition was minimal even as a low time pilot. Also keep in mind that if you do something really unique you may limit resale. I looked at one plane that had the primary instruments on the right side. That in addition to everything being red was a deal breaker for me. But do whatever makes you happy. Ron Lee ________________________________________________________________________________
From: "Ed Holyoke" <bicyclop(at)pacbell.net>
Subject: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
When I got out of a Cessna and into an RV-6a, speed control was the issue I was concentrating on and the stick never felt funny for a minute. It felt natural in my left hand from the start. Yokes and high wings are just wrong. I'm building a six with a center quadrant. Ed Holyoke 6a (built by another) 6 under construction -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Paul Folbrecht Subject: Re: RV-List: Control sticks with bend/left-hand throttle quadrant No trouble initially, either? It didn't take getting used to? It is funny that flying a yoke with my left is completely natural yet I know (or think I know) that a stick in my left and will not feel that way. Maybe that's just because my very, very limited "_stick_ time" has been with my right. If that's the case, I should be used to the left in < 2 hours. > I am right handed and fly the RV-6A with my left hand with NO problem. > Actually I think flying with my right hand would be odd. ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: Apr 29, 2005
Subject: 3/16 rivets and a 2X gun
Hi all I have been looking at the lone 3/16 (fixed a boo-boo) rivet that I have to install in my forward HS spar. I have a 2X rivet gun. I have done a pile of practice rivets. The 2X drives the rivet okay, if a little slow. Someone had said that they wouldn't use less than a 4X gun for that size rivet. What exactly is the difference? Is there a bigger weight being popped by the pneumatics? Besides being slower, is there an important disadvantage or problem associated with using my gun? I would hate to buy another gun for one rivet. Thanks Michael Wynn RV-8, Empennage San Ramon, California ________________________________________________________________________________
Date: Apr 28, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Control sticks with bend/left-hand throttle quadrant
What type of center quadrant? I've decided I'm sure I can be trained to fly LH stick. Which means a center engine quadrant makes sense (I'd just rather not have the engine controls on the panel). --- Ed Holyoke wrote: > > When I got out of a Cessna and into an RV-6a, speed control was the > issue I was concentrating on and the stick never felt funny for a > minute. It felt natural in my left hand from the start. Yokes and high > wings are just wrong. I'm building a six with a center quadrant. > > Ed Holyoke > 6a (built by another) > 6 under construction > ________________________________________________________________________________
Date: Apr 29, 2005
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: 3/16 rivets and a 2X gun
Michael; How long is the rivet in question? I managed OK driving shorter 3/16 AN rivets with a lighter weight gun but was simply unable to drive the longer ones in an RV-6 spar. I eventually used a C-frame riveter, a 470-6 set, and a five pound hammer with good results. Just make sure everything is lined up, lean on the spar to hold it in place and pound away. Jim Oke RV-6A Wpg., MB ----- Original Message ----- From: <MLWynn(at)aol.com> Subject: RV-List: 3/16 rivets and a 2X gun > > Hi all > > I have been looking at the lone 3/16 (fixed a boo-boo) rivet that I have > to > install in my forward HS spar. I have a 2X rivet gun. I have done a pile > of > practice rivets. The 2X drives the rivet okay, if a little slow. Someone > had > said that they wouldn't use less than a 4X gun for that size rivet. What > exactly is the difference? Is there a bigger weight being popped by the > pneumatics? > > Besides being slower, is there an important disadvantage or problem > associated with using my gun? I would hate to buy another gun for one > rivet. > > Thanks > > Michael Wynn > RV-8, Empennage > San Ramon, California > > > ________________________________________________________________________________
From: "Ed Holyoke" <bicyclop(at)pacbell.net>
Subject: Control sticks with bend/left-hand throttle quadrant
Date: Apr 28, 2005
Paul, It looks like (and is made by the same guy as) this: http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1114751560-466-705 &browse=controls&product=10-quadrant I'll post a picture of how I mounted it in a day or two. Ed Holyoke -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Paul Folbrecht Subject: RE: RV-List: Control sticks with bend/left-hand throttle quadrant What type of center quadrant? I've decided I'm sure I can be trained to fly LH stick. Which means a center engine quadrant makes sense (I'd just rather not have the engine controls on the panel). --- Ed Holyoke wrote: > > When I got out of a Cessna and into an RV-6a, speed control was the > issue I was concentrating on and the stick never felt funny for a > minute. It felt natural in my left hand from the start. Yokes and high > wings are just wrong. I'm building a six with a center quadrant. > > Ed Holyoke > 6a (built by another) > 6 under construction > ________________________________________________________________________________
Date: Apr 29, 2005
From: Jim Oke <wjoke(at)shaw.ca>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
If you intend to do most of your flying from the right seat, why not put the primary flight instruments on the right side of the panel? I did. See http://www.vansairforce.org/projects/okej/onephoto.cgi?Picture_0630.jpg The throttle mount in the centre of the panel keeps the throttle at your left hand and is much simpler and lighter than trying to add a second throttle on the left side of the cockpit. Jim Oke ----- Original Message ----- From: "son hoang" <son(at)hoangs.com> Subject: Re: RV-List: Control sticks with bend/left-hand throttle quadrant > > easy solution > fly from the right seat > all CFI do it daily > > ----- Original Message ----- > From: "Paul Folbrecht" <paulfolbrecht(at)yahoo.com> > To: > Subject: RV-List: Control sticks with bend/left-hand throttle quadrant > > >> >> Two unrelated questions: >> >> 1) I know I have seen RVs with control sticks with a forward bend in >> them. > I >> want them cause they look much cooler than the straight sticks. Who >> makes >> them? >> >> 2) It seems it's pretty customary to put the engine controls on the >> panel, >> meaning used with right hand, which I assume means stick in left hand. >> Of >> course I fly yoke-equipped planes with my left on the yoke but I think > that >> using my right hand on a control stick might be far more natural (I am >> right-handed, like all good Americans*). The only time I have in >> stick-controlled aircraft is my RV-10 demo ride and a couple flights in a >> Challenger UL, and in both cases I used my right on the stick. >> >> With those thoughts, I was thinking that a left-hand engine-control > arrangement >> might really be ideal. Thoughts on this?? Does anyone make an > aftermarket >> side-mounted throttle-quadrant. Should I just learn to fly with my left > hand >> on the stick like everybody else? >> >> * Just kidding. >> >> > > > ________________________________________________________________________________
From: "Jim Jewell" <jjewell(at)telus.net>
Subject: Re: 3/16 rivets and a 2X gun
Date: Apr 28, 2005
Hi Michael, You could drive the single rivet with a hammer. To do this an extra set of hands and eyes and a carefully controlled set up should get good results. You could avoid the issue of driving the "one rivet" by installing a Cherry-Max structural pull rivet instead. You can read about this kind of fastener and the aircraft industries many others in a book called "Standard Aircraft Handbook" published by McGraw Hill. I have the fifth edition #3634. If you don't have a copy get one , it will be worth the price. It is full of descriptions of fasteners, the tools needed for them, how to use the tools and lots of reference charts, conversions tables etc. It reads slightly better that the phone book until you need it, Then it gets Quite interesting. I got my copy from Van's Rivets are designed (alloyed) soft before being driven. The driving process work hardens them. If over worked (driven too long or too much) they can become too brittle. Rivets driven by under sized guns tend not to look finished right and can be unsound in certain structural high load conditions or locations. From the book; "always select a rivet gun size and bucking bar weight that drive the rivet with as few blows as possible". The various rivet guns bores and or strokes increase as the gun # goes up. The bigger guns hit harder and less often per minute. In actual use the utility of the guns tends to overlap some of the rivet sizes. Generally a #2 gun will drive 3/32" and 1/8" rivets quite well. Driving 3/16" rivets with a # 2 gun is near (if not) the limit. A #3 gun can be set up to drive #/32", 1/8" and 3/16" rivets. A # 4 gun will tend to be a bit too powerful to use on 3/32" rivets (damage to surrounding stucture can result) but can drive rivets bigger than 3/16" and so on. At some point personal preference enters the scene. Some RV builders prefer the # 2 guns and others will swear by #3 guns and so on. The #3 gun is physically larger and a bit heavier but it reaches the range of rivet sizes generally found in single and two place home builds quite well. Keep on driving em, Jim in Kelowna ----- Original Message ----- From: <MLWynn(at)aol.com> Subject: RV-List: 3/16 rivets and a 2X gun > > Hi all > > I have been looking at the lone 3/16 (fixed a boo-boo) rivet that I have > to > install in my forward HS spar. I have a 2X rivet gun. I have done a pile > of > practice rivets. The 2X drives the rivet okay, if a little slow. Someone > had > said that they wouldn't use less than a 4X gun for that size rivet. What > exactly is the difference? Is there a bigger weight being popped by the > pneumatics? > > Besides being slower, is there an important disadvantage or problem > associated with using my gun? I would hate to buy another gun for one > rivet. > > Thanks > > Michael Wynn > RV-8, Empennage > San Ramon, California > > > ________________________________________________________________________________
Date: Apr 29, 2005
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: Belt Sander Question & Tool Resource
I'd go for at least the 4 inch wide belt model at a minimum, and bigger if you can afford it. They are great for shaping parts (poor mans mill.) You do still have to shape parts on the 7, don't you? ') Jeff Point RV-6 Milwaukee WI >Craftsman has a 2x42" belt / 6" disc unit that looks >nice... will it do the job? > > > > ________________________________________________________________________________
From: PSILeD(at)aol.com
Date: Apr 29, 2005
Subject: Re: Control sticks with bend/left-hand throttle quadrant
try www.rvwoody.com, he may not be doing iy anymore but he certainly does excellent work. Paul ________________________________________________________________________________
From: "Kevin Williams" <kevinsky18(at)hotmail.com>
Subject: Re: Best website for posting builder log
Date: Apr 29, 2005
I'm gearing up to start my project and want to get my builder log / webpage started. My ISP doesnt provide webspace. What other cheap / free sites are out there that will let me post lots of pictures ect and be relatively user friendly. Kevin Yellowknife, NT, Canada RV-8 Wanna Be Builder ________________________________________________________________________________
From: "tpu2(at)juno.com" <tpu2(at)juno.com>
Date: Apr 29, 2005
Subject: RV builders clinic
An Indianapolis area builders assistance center is now conducting Basic RV construction builders clinics. The first one is May 21-22. Details are available at rv6grover(at)netzero.net or 317-919-6594. ________________________________________________________________________________
From: "Speed 3 Guy" <speed3guy(at)comcast.net>
Subject: Best website for posting builder log
Date: Apr 29, 2005
Kevin, I really like www.expercraft.com. It's free and simple. Here's a link to my site on expercraft: http://websites.expercraft.com/geprevo/ Guy I'm gearing up to start my project and want to get my builder log / webpage started. My ISP doesnt provide webspace. What other cheap / free sites are out there that will let me post lots of pictures ect and be relatively user friendly. Kevin Yellowknife, NT, Canada RV-8 Wanna Be Builder ________________________________________________________________________________
Date: Apr 29, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: 7(A) vs. 9(A) for XC flying
I'm not asking a "decide-what-to-build" q here because my 7A quickbuild kit is ordered and that's what I want. (I want the slightly better speed than the 9, the ability to go 180hp, and, although I don't know if I'll ever actually want to do "genleman's aerobatics" (I'm no gentleman, I've been told), I want to retain that capability too.) But, anyway, I see it thrown around a lot that the 9(A) is a "better" XC machine than the 7(A), and I don't know if I buy that. Stability is touted. I haven't flown in a 9, but it seems to me that the shorter wing and slightly higher loading of the 6/7 might well offset any inherently better pitch stability of the 9. If the 6/7 holds pitch well when trimmed, which definitely seems to be the case, that's what's really important. Any airplane needs attention to the roll axis or it's going to wander into a spiral. Seems to me that what's more important is stability in chop and turbulence and the 7 ought to do slightly better there. Thoughts? ________________________________________________________________________________
Subject: Lefties Flying Right Handed
Date: Apr 29, 2005
From: "Valovich, Paul" <pvalovich(at)dcscorp.com>
I'm a lefty - can't seem to do anything right handed. However, the Navy taught me to fly with the throttle in my left hand and the stick in my right. No problems - at least in becoming accustomed to the feel and function of right handed tasking. There was a meaningless line going around when I was in flight training: If upon entering the cockpit you find the throttle in your right hand and the stick up your butt, you've climbed in backwards. Paul Valovich RV-8A QB fus & wings delivered last Wednesday ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Best website for posting builder log
Date: Apr 29, 2005
I have used both Geo-Cities and Tripod. I just googled free websites and this is a good source. http://www.freewebsiteproviders.com Cy Galley - Bellanca Champion Club Newsletter Editor-in-Chief & EAA TC www.bellanca-championclub.com Actively supporting Bellancas every day ----- Original Message ----- From: "Kevin Williams" <kevinsky18(at)hotmail.com> Subject: Re: RV-List: Best website for posting builder log > > I'm gearing up to start my project and want to get my builder log / > webpage > started. My ISP doesnt provide webspace. What other cheap / free sites > are out there that will let me post lots of pictures ect and be relatively > user friendly. > > > Kevin > > Yellowknife, NT, Canada > RV-8 Wanna Be Builder > > > ________________________________________________________________________________
Date: Apr 29, 2005
From: Bobby Hester <bhester(at)hopkinsville.net>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
PSILeD(at)aol.com wrote: > >try www.rvwoody.com, he may not be doing iy anymore but he certainly does >excellent work. >Paul > > > Here is the direct link to the bent stick: http://www.rvwoody.com/Stick.html -- Surfing the Web from Hopkinsville, KY Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ RV7A Slowbuild wings-QB Fuse :-) ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: Apr 29, 2005
Subject: Re: Belt Sander Question & Tool Resource
In a message dated 4/28/05 1:02:09 PM Pacific Daylight Time, brad(at)rv7factory.com writes: > My question is, in purchasing a belt sander, are their particular features > I should look for or stay away from? Craftsman has a 2x42" belt / 6" disc > unit that looks > nice... will it do the job? > I used a one inch Craftsman belt sander with the finest grit I could buy from day one on my RV-6 and found it to be one of the most useful tools I had. I never had a need for a wider belt and never used the disc sander part of the tool, but that's just me. Harry Crosby RV-6 N16CX, 68 hours ________________________________________________________________________________
Date: Apr 29, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: Control sticks with bend/left-hand throttle quadrant
That stick looks nice but it's not the one I'd seen - that one had a very wide, forward "C" bend, very similar to the sticks in an OMF Symphony, if you've ever seen one of those. The shape keeps your lap free with the stick out of the way. --- Bobby Hester wrote: > > PSILeD(at)aol.com wrote: > > > > >try www.rvwoody.com, he may not be doing iy anymore but he certainly does > >excellent work. > >Paul > > > > > > > Here is the direct link to the bent stick: http://www.rvwoody.com/Stick.html > > -- > Surfing the Web from Hopkinsville, KY > Visit my web site at: http://www.geocities.com/hester-hoptown/RVSite/ > RV7A Slowbuild wings-QB Fuse :-) > > > > > > > > ________________________________________________________________________________
Date: Apr 29, 2005
Subject: Re: 3/16 rivets and a 2X gun
From: "Jamie Painter" <jdpainter(at)jpainter.org>
> I have been looking at the lone 3/16 (fixed a boo-boo) rivet that I have to > install in my forward HS spar. I have a 2X rivet gun. I have done a pile of > practice rivets. The 2X drives the rivet okay, if a little slow. Someone had > said that they wouldn't use less than a 4X gun for that size rivet. What > exactly is the difference? Is there a bigger weight being popped by the > pneumatics? Michael: Riveting the 3/16 rivets with a 2x will work OK in certain materials, but for example on the wing rib to spar rivets, where you have the relatively thick spar web material, you may find it very difficult to set them (seems that the thicker material absorbs some of the impact force from the gun). I had a lot of trouble doing this with my 2x, so I bought a 3x. For me, it made a world of difference. Other folks have said that they used the 2x without a problem. I now switch back and forth between the 2x and 3x guns. I generally use the 2x on 3/32nd rivets and the 3x on the 3/16. But on the bottom skins for example, where you are holding the bucking bar with a contorted wrist, I found the 3x to be better for the 3/32nds simply because it didn't take as long to set the rivets. As always, your mileage will vary. Hope that helps, Jamie -- Jamie D. Painter RV-7A fuselage N622JP (reserved) http://rv.jpainter.org ________________________________________________________________________________
Date: Apr 29, 2005
From: Richard Scott <rscott(at)cascadeaccess.com>
Subject: 7(A) vs. 9(A) for XC flying
All I know is that when I ordered my 9 tail kit, Tom Green told me that whenever the company folks went X-C, if they had their choice, they ALL took the 9. That was before the 10 was flying. Richard Scott 9A Wings ________________________________________________________________________________
Date: Apr 29, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: 7(A) vs. 9(A) for XC flying
Blah! I've been doing my homework and obviously the 9 is going to be an easier-to-fly IFR bird, with 3x the stick force for one thing. I sent my 7A QB order form in yesterday. Well, it's certainly not too late. I can call them on Monday. I am waiting for 2 months for shipping for my house to be done anyway. I will probably call them and ask them to hold off altogether for a bit. "Easy" IFR flying means a lot more to me than 10mph and aerobatic capability I will probably never use. Funny thing is the 9A is the first kitplane I ever wanted. If I end up building one, I have certainly come full circle. --- Richard Scott wrote: > > All I know is that when I ordered my 9 tail kit, Tom Green told me that > whenever the company folks went X-C, if they had their choice, they ALL > took the 9. That was before the 10 was flying. > > > Richard Scott > 9A Wings > > > > > > > > ________________________________________________________________________________
From: "James Ochs" <jochs(at)froody.org>
Subject: AFS (Aircraft Finishing Systems) stuff for corrosion protection
Date: Apr 29, 2005
Hi Paul and list, Check out Sanchem, http://www.sanchem.com I bought the 6100 product and seal #2 and it is very easy to use, very easy to clean up and environmentally friendly. It is a direct replacement for alodine, and seal #2 is a replacement for primer. They have results from testing on their site that compares it's performance to alodine and a couple of other products. The seal #2 puts a fairly tough layer what looks like a hard, clear plastic or enamel on top of the metal. I bought the product and have tested it on some small scraps and it seems to perform as advertised and give good surface for priming and a solid seal if you are not priming. Obviously I won't know what the corrosion performance is in my application for a few years since I don't have a lab setup, but after spending some time on the phone with them I feel confident that they know what they are doing. If anyone has experience with the product, please let me know what you thought of it as I am getting started shortly with my project ;) If anyone is interested, I have the MSDS, instructions and pricing info so just email me off-list and I can forward them to you. James #40400 Waiting on the emp. Kit -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Paul Folbrecht Subject: RV-List: AFS (Aircraft Finishing Systems) stuff for corrosion protection I'm doing a QB RV-7A but still need to decide on a corrosion protected mechanism for the tail. I am really interestd in the AFS stuff for its non-toxic qualities. A search of the archive provided few hits re: priming/corrosion protection with this stuff. Has anybody used the AFS stuff or know somebody that did? Did you use all three of the products - cleaner, etch, primer? Is it possible to apply the primer by dipping parts in a tub or does it need to be sprayed HVLP? ________________________________________________________________________________
Date: Apr 30, 2005
Subject: 9 vs 6 experience
From: WALTER B KERR <jbker(at)juno.com>
I have built both and flew the 6A 400 + hours mostly CC, no aerobatics. Now have flown the 9A for 30 hours and it definitely is more stable( OK ,less responsive to you jet jock types). Tom Green and Van both concede that it is more comfortable on long CC. I have not mastered getting it to land as accurately as the 6. The thing just will not tolerate extra speed or it will not quit flying compared to the 6A which bled speed rapidly on the backside of the power curve. Bernie Kerr, 13B Mazda in my 9A Blah! I've been doing my homework and obviously the 9 is going to be an easier-to-fly IFR bird, with 3x the stick force for one thing. I sent my 7A QB order form in yesterday. Well, it's certainly not too late. I can call them on Monday. I am waiting for 2 months for shipping for my house to be done anyway. I will probably call them and ask them to hold off altogether for a bit. "Easy" IFR flying means a lot more to me than 10mph and aerobatic capability I will probably never use. Funny thing is the 9A is the first kitplane I ever wanted. If I end up building one, I have certainly come full circle. --- Richard Scott wrote: > > All I know is that when I ordered my 9 tail kit, Tom Green told me that > whenever the company folks went X-C, if they had their choice, they ALL > took the 9. That was before the 10 was flying. > > > Richard Scott > 9A Wings ________________________________________________________________________________
Date: Apr 30, 2005
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: magneto's check on EIS
Do you have two mags or one mag and an electronic ignition? How is the switch wired? The EIS RPM input from the mag P lead requires a resister between it and the mag. I managed to screw this up the first time I wired mine,and putting a switch in there would make it more complicated. I'd check that first. If you're using the same input for both (through the switch) than the problem is obviously not with the EIS. Jeff Point RV-6 Milwaukee WI > > ________________________________________________________________________________
From: MLWynn(at)aol.com
Date: Apr 30, 2005
Subject: Re: AFS (Aircraft Finishing Systems) stuff for corrosion protection
Hi James I have no experience with this system. However, having read through their data, it looks like a really good substitution for Alodine. I have been concerned about the toxicity of alodine and how to dispose of the leavings. If this stuff works as advertised, it would be an excellent substitution. I am assuming from the website that one would do the standard steps of clean with MEK or acetone, prep with Alumaprep or similar, follow with Safeguard CC 3000 or so and then prime as per usual. Anyone with thoughts or experience? Regards, Michael Wynn RV-8, Empennage San Ramon, California ________________________________________________________________________________
From: "James Ochs" <jochs(at)froody.org>
Subject: AFS (Aircraft Finishing Systems) stuff for corrosion protection
Date: Apr 30, 2005
Actually, the 3000 system is designed to be applied hot and in tanks... the 6100 system is the one I am using and doesn't need any special treatment other than mixing part a and part b and brushing or spraying it on. As far as cleaning the 6100 process comes with part A, part B and part C. The application process is to clean with part C (also non toxic and very effective) using a scotchbrite pad, then rinse with deionized or distilled water, dry, put on the part a part b mix (they mix 1:1) wait about 60 seconds until it turns gold, and then rinse again. If you don't get the color change then it wasn't cleaned enough and you start over. If you want to use the sealer, then you brush that on and hit it with a heat gun for about a minute and it puts a nice solid clear coat of what almost looks like plastic on top. No need for MEK or acetone or any of that other fun stuff ;) I'll send you the MSDS and instructions off list. James #40400 -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of MLWynn(at)aol.com Subject: Re: RV-List: AFS (Aircraft Finishing Systems) stuff for corrosion protection Hi James I have no experience with this system. However, having read through their data, it looks like a really good substitution for Alodine. I have been concerned about the toxicity of alodine and how to dispose of the leavings. If this stuff works as advertised, it would be an excellent substitution. I am assuming from the website that one would do the standard steps of clean with MEK or acetone, prep with Alumaprep or similar, follow with Safeguard CC 3000 or so and then prime as per usual. Anyone with thoughts or experience? Regards, Michael Wynn RV-8, Empennage San Ramon, California ________________________________________________________________________________
Date: Apr 30, 2005
From: Paul Trotter <ptrotter(at)acm.org>
Subject: Aluminum Air Vents
I don't particularly like the plastic eyeball vents that Vans supplies and would like to use aluminum vents instead. I recall seeing several units advertised but can't seem to remember where. Does anybody know who has these at a better price than the normal places like Spruce? Thanks, Paul RV-8 ________________________________________________________________________________
Date: Apr 30, 2005
From: rv6fly <rv6fly(at)bresnan.net>
Subject: Re: Aluminum Air Vents
Paul Trotter wrote: > >I don't particularly like the plastic eyeball vents that Vans supplies and >would like to use aluminum vents instead. I recall seeing several units >advertised but can't seem to remember where. Does anybody know who has >these at a better price than the normal places like Spruce? > > > I agree, Paul. On my six, I used alum. eyball vents that I bought from an a/c/ salvage yard as opposed to the much more costly vents that you can buy at Spruce. I believe they were out of a Cessna 400. Be carefull if you order from a salvage yard that you don't end up with something smaller like what's used on passenger planes above the seat. I don't think they'd flow as much air. To make an adapter for the hose at the rear of the vent, I turned down a bit (tapered) and polished a regular, 2" flanged duct, waxed it and layed up fiberglass on it whenever I had some left over. You can then glue them on the back with J-B weld, Proseal, etc. Bob Skinner -- ________________________________________________________________________________
Subject: magneto's check on EIS
Date: Apr 30, 2005
From: "Greg Young" <gyoung@cs-sol.com>
If you have the tach pickup wired to the P-lead of one mag you'll only get a reading when that mag is on. When you turn it off during the mag check the RPM will go to zero. It's OK to just do your mag check by comparative sound. If you don't like that you can get a tach generator to feed the EIS input instead of using the P-lead. Vans has them, including one with an extended cable if you need clearance from a vacuum pump. Regards, Greg Young - Houston (DWH) RV-6 N6GY ...project Phoenix Navion N5221K - just an XXL RV-6A > > > Hi: > > > Any one with the E.I.S. From Grand Rapids, might know the > answer to my question. > > When I am doing the run-up, and check Mags, for drop..the > Engine Monitor shows Zero...when switching from L to R. > > Of course I change the INdividual switch one has, up for > the L and down for the R mag.. > > Otherwise everything shows OK.. > > Any answers to this ? > > > Thanks > > Bertrv6a > > Starting my Flight Test... > ________________________________________________________________________________
From: Dwpetrus(at)aol.com
Date: Apr 30, 2005
Subject: Re: magneto's check on EIS
or get a switch to switch to either mag for mag check. ________________________________________________________________________________
Date: Apr 30, 2005
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: Aluminum Air Vents
B & B aircraft has some which are larger than the ones normally seen, about 3 inches or so. B&B AIRCRAFT SUPPLIES 913-884-5930 AN HARDWARE, AIRCRAFT SURPLUS AND LEATHER SEAT SKINS I got mine from Wicks, which are smaller than the Van's plastic ones, but at RV speeds they allow plenty of airflow. http://www.wicksaircraft.com/catalog/product_cat.php/subid=2839/index.html Jeff Point > > ________________________________________________________________________________
Date: Apr 30, 2005
From: Charlie Kuss <chaztuna(at)adelphia.net>
Subject: Re: Aluminum Air Vents
Paul Local RV-9A builder Fabian Lefler owns AFFORDABLE PANELS.com Fabian designed and is marketing a very nice aluminum vent the same size as Vans. His price is better than most of the other aluminum vents I've seen. See http://www.affordablepanels.com/aluminum_vents.htm Charlie Kuss > >I don't particularly like the plastic eyeball vents that Vans supplies and >would like to use aluminum vents instead. I recall seeing several units >advertised but can't seem to remember where. Does anybody know who has >these at a better price than the normal places like Spruce? > >Thanks, > >Paul >RV-8 > > ________________________________________________________________________________
From: "Stein Bruch" <stein(at)steinair.com>
Subject: Aluminum Air Vents
Date: Apr 30, 2005
Ummm....not really - Sometimes people take credit for things that they shouldn't.... Anyway, these vents are actually made by a company called "Airkit, LLC". The same Vents are sold for the same price by a lot of people, including Van's Aircraft (http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1114912044-64-423&bro wse=heatvent). I actually looked into stocking them, but with such a small company like Airkit and not a lot of margin, I figured I'd just point people to the companies website (http://www.airkitllc.com) and tell people to buy them direct for only $5.00 more. I like to see small business like that succeed so I throw as much business directly to them as I can! Those are nice vents but pretty large. I use the standard sized Wemac Aluminum vents in both my RV's and like them the best. I've used the large ones, but IHMO, they aren't quite as nice overall as the smaller ones when it comes to directing airflow. I like to direct a stream of air onto my face, chest or forehead when I like, and the smaller 1.5+" ones work best for me. You can get them for $50+ something at ACS or other places, but my personal favorite place is just digging through an aircraft junkyard (like Wentworth) until you find some you need. They usually sell them for much less. Just my 2 cents as usual! Cheers, Stein. P.S., no flames intended. -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Charlie Kuss Subject: Re: RV-List: Aluminum Air Vents Paul Local RV-9A builder Fabian Lefler owns AFFORDABLE PANELS.com Fabian designed and is marketing a very nice aluminum vent the same size as Vans. His price is better than most of the other aluminum vents I've seen. See http://www.affordablepanels.com/aluminum_vents.htm Charlie Kuss > >I don't particularly like the plastic eyeball vents that Vans supplies and >would like to use aluminum vents instead. I recall seeing several units >advertised but can't seem to remember where. Does anybody know who has >these at a better price than the normal places like Spruce? > >Thanks, > >Paul >RV-8 > > ________________________________________________________________________________
From: "Michel" <rv8ter(at)rogers.com>
Subject: Aluminum Air Vents
Date: Apr 30, 2005
I found the rear vent leak cold air in the winter even after putting the PRC to seal the door and when Van's came out with these fancy expensive Aluminum ones I had to replace my plastic cheapee. Well the rear vent air intake is in the prop blast and particularly in the climb the looseness in the vent valve makes such a rattling noise that it overpowers my Bose ANR. I have just reinstalled the plastic unit after spending the winter with the under wing vent taped up. Just a fair warning. Michel C-GERV 81117 470 hrs -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Charlie Kuss Subject: Re: RV-List: Aluminum Air Vents Paul Local RV-9A builder Fabian Lefler owns AFFORDABLE PANELS.com Fabian designed and is marketing a very nice aluminum vent the same size as Vans. His price is better than most of the other aluminum vents I've seen. See http://www.affordablepanels.com/aluminum_vents.htm Charlie Kuss > >I don't particularly like the plastic eyeball vents that Vans supplies and >would like to use aluminum vents instead. I recall seeing several units >advertised but can't seem to remember where. Does anybody know who has >these at a better price than the normal places like Spruce? > >Thanks, > >Paul >RV-8 > > ________________________________________________________________________________
Date: Apr 30, 2005
From: Mark Grieve <mark(at)macomb.com>
Subject: Re: AFS (Aircraft Finishing Systems) stuff for corrosion
protection Paul, The original builder of my empennage used AFS. I read up on the product and it seems to have a lot going for it. I like the non-toxic aspect but the warm water cleanup really appeals to me. Also, being one part, you have the option of storing the unused primer for the next session. AFS says you can dump it right back into the can but I'm not sure I would. The possibility of contamination scares me just a little. The primer can be applied in any manor you see fit, spray, brush, dip, squirt or splatter. I would suggest spraying as it will produce the most even coat. AFS suggests spraying, brushing or rolling. The pieces I have were brushed and the coat is pretty uneven but a second coat would help that. Dipping may be OK for applying the conversion coating but I wouldn't apply the primer that way. The result will be a very thick coat that is uneven as the part drains. There will also be drips at the lowest point and you would waste a lot of product. This stuff isn't cheap! It takes a few days for the primer to dry/cure and it isn't very durable during this period. Very easy to scrape off. Once cured it seems pretty durable and doesn't flake when you dimple. I have gone back to make sure the spars are deburred and the primer doesn't flake off of the adjacent surfaces. For spraying, a touch up gun is what AFS suggests. I believe HVLP is mandatory if you live in California. Here in Illinois we aren't so enlightened so hold your breath Indiana! If you have never used a gun before then get a quart of latex house paint off the shelf in the basement, thin it down to be the same as the primer and practice till you get the feel of it. A simple spray booth can be made using a large cardboard box and some safety wire. Regardless of application method you will need a good respirator because this stuff smells horrible! You should be wearing a mask no matter what kind of primer you apply so this isn't a bid deal. There was a discussion of AFS on the RV-7 list last fall I believe. You might find something in that archive if you haven't searched already. Happy priming Mark Paul Folbrecht wrote: >I am really interestd in the AFS stuff for its non-toxic qualities. A search >of the archive provided few hits re: priming/corrosion protection with this >stuff. > >Has anybody used the AFS stuff or know somebody that did? Did you use all >three of the products - cleaner, etch, primer? Is it possible to apply the >primer by dipping parts in a tub or does it need to be sprayed HVLP? > > ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Garmin 196 Obstacle
Date: Apr 30, 2005
I installed the latest update for the Garmin 196, eager to check out the obstacle functionality. It says "Obstacle data not present" or something to that effect, on start-up. I have the 0412 database. I don't see reference to a minimum database version on their website. Does anyone know? - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com ________________________________________________________________________________
From: "Michael Hilger" <rvsixer(at)juno.com>
Subject: Re: Garmin 196 Obstacle
Date: Apr 30, 2005
----- Original Message ----- From: "Larry Bowen" <Larry(at)bowenaero.com> Subject: RV-List: Garmin 196 Obstacle I installed the latest update for the Garmin 196, eager to check out the obstacle functionality. It says "Obstacle data not present" or something to that effect, on start-up. I have the 0412 database. I don't see reference to a minimum database version on their website. Does anyone know? Larry, The obstacle database is a seperate download from the database updates (not free, either, but worth it). You also have to update the operating software, and that is free from Garmin (if you haven't already). Mike Hilger RV-6 N207AM 700 hrs ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: 3/16 rivets and a 2X gun
Date: May 01, 2005
I have built my entire plane using only a 2X gun. It works and is lighter in weight. A 3X gun will work also but be a bit heavier. The 2X gun works but may take a two or three seconds when working on rivets surrounded by heavy structure. You don't need a heavier gun with Van's RV8 kit. Indiana Larry, RV7 Tip Up FLYING - Phase 1 Test ----- Original Message ----- From: <MLWynn(at)aol.com> Subject: RV-List: 3/16 rivets and a 2X gun > > Hi all > > I have been looking at the lone 3/16 (fixed a boo-boo) rivet that I have > to > install in my forward HS spar. I have a 2X rivet gun. I have done a pile > of > practice rivets. The 2X drives the rivet okay, if a little slow. Someone > had > said that they wouldn't use less than a 4X gun for that size rivet. What > exactly is the difference? Is there a bigger weight being popped by the > pneumatics? > > Besides being slower, is there an important disadvantage or problem > associated with using my gun? I would hate to buy another gun for one > rivet. > > Thanks > > Michael Wynn > RV-8, Empennage > San Ramon, California > > > ________________________________________________________________________________
From: "Charles Heathco" <cheathco(at)comcast.net>
Subject: Long glide to landing
Date: May 01, 2005
Last Thur we had a rare exelent flying day, I thought I would try to hit Jax county from 10 miles out and 5000' strait in (I keep an anouncment going, no one in the pattern) I thought I was doing pretty good untill I got about mile and half out, looked like overshoot so did some slow s's, then steep slip, but only got to pattern altitude at about short final, gave it up. I hadnt tried this since I got my coml long time ago. Yhis was in my 6a. I think this would be good practice and wondered if any of you do this, and what is your procedure? This might be of intrest to otheres as well. Charlie heathco ________________________________________________________________________________
Date: May 01, 2005
From: Bob J <rocketbob(at)gmail.com>
Subject: Re: Aluminum Air Vents
Jeff Mears (aka Airkit LLC) is a friend of mine and an RV-6A driver. He supplies these to Van's, AC$, Affordable Panels, etc. and also sells them directly. He has continually made improvements to the vents, the latest generation work very smoothly and seal better than the previous generations. He has also developed some new sizes of vents, one of which is designed to work in a 2" hole with a screwed-on piece behind the panel which accepts a 2" scat tube. The website should be updated within the next few days showing these new models. Regards, Bob Japundza RV-6 flying 600+ hours F1 under const. On 4/30/05, Stein Bruch wrote: > > Ummm....not really - Sometimes people take credit for things that they > shouldn't.... > > Anyway, these vents are actually made by a company called "Airkit, LLC". > The same Vents are sold for the same price by a lot of people, including > Van's Aircraft > (http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1114912044-64-423&bro > wse=heatvent). I actually looked into stocking them, but with such a small > company like Airkit and not a lot of margin, I figured I'd just point people > to the companies website (http://www.airkitllc.com) and tell people to buy > them direct for only $5.00 more. I like to see small business like that > succeed so I throw as much business directly to them as I can! > > Those are nice vents but pretty large. I use the standard sized Wemac > Aluminum vents in both my RV's and like them the best. I've used the large > ones, but IHMO, they aren't quite as nice overall as the smaller ones when > it comes to directing airflow. I like to direct a stream of air onto my > face, chest or forehead when I like, and the smaller 1.5+" ones work best > for me. You can get them for $50+ something at ACS or other places, but my > personal favorite place is just digging through an aircraft junkyard (like > Wentworth) until you find some you need. They usually sell them for much > less. > > Just my 2 cents as usual! > > Cheers, > Stein. > > P.S., no flames intended. > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Charlie Kuss > To: rv-list(at)matronics.com > Subject: Re: RV-List: Aluminum Air Vents > > > Paul > Local RV-9A builder Fabian Lefler owns AFFORDABLE PANELS.com Fabian > designed and is marketing a very nice aluminum vent the same size as Vans. > His price is better than most of the other aluminum vents I've seen. See > > http://www.affordablepanels.com/aluminum_vents.htm > > Charlie Kuss > > > > >I don't particularly like the plastic eyeball vents that Vans supplies and > >would like to use aluminum vents instead. I recall seeing several units > >advertised but can't seem to remember where. Does anybody know who has > >these at a better price than the normal places like Spruce? > > > >Thanks, > > > >Paul > >RV-8 > > > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Long glide to landing
Date: May 01, 2005
Depends on what you are trying to achieve, Charles If I am practicing "engine out" then my procedure is to "save" every bit of altitude I can and arrive over the airfield with as much altitude remaining as possible. Then depending on altitude, I do a couple of tight 360 deg turns combined with additional "S" turns if necessary to loose sufficient altitude. I come in higher and a bit faster on final than normal. My personal philosophy is I would rather go off the far end of the runway at 20 mph than find myself short on airspeed and altitude on the arrival end of the runway. If I am doing long straight-in approaches (which I do not normally do), I mentally calculate from my desired descent airspeed how long it would take me to get to the airport from my start descent position. Then I estimate what rate of descent would get me to pattern altitude in the time I calculated. And if I hold those parameters I find I generally arrive with close approximation to the altitude I expected (with perhaps some adjustments on the way down for wind, other factors, etc). My Garmin 195 has a Vertical Nav mode whereby you can specify your desired altitude at destination and desired rate of descent and then just fly the descent bar when the system tells when you are at your start descent point - quite accurate. It calculates where you need to start your descent based on altitude, groundspeed and specified rate of descent and then notifies you when you are approach your start descent point. Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC 28104 ----- Original Message ----- From: "Charles Heathco" <cheathco(at)comcast.net> Subject: RV-List: Long glide to landing > > Last Thur we had a rare exelent flying day, I thought I would try to hit > Jax county from 10 miles out and 5000' strait in (I keep an anouncment > going, no one in the pattern) > I thought I was doing pretty good untill I got about mile and half out, > looked like overshoot so did some slow s's, then steep slip, but only got > to pattern altitude at about > short final, gave it up. I hadnt tried this since I got my coml long time > ago. Yhis was in my 6a. I think this would be good practice and wondered > if any of you do this, and what is your procedure? This might be of > intrest to otheres as well. Charlie heathco > > > ________________________________________________________________________________
From: "Larry Bowen" <Larry(at)bowenaero.com>
Subject: Aluminum Air Vents
Date: May 01, 2005
If you are not in a hurry, the best deals for these vents are on eBay. I've bought several there. - Larry Bowen Larry(at)BowenAero.com http://BowenAero.com > -----Original Message----- > >I don't particularly like the plastic eyeball vents that Vans >supplies and would like to use aluminum vents instead. I recall >seeing several units advertised but can't seem to remember where. >Does anybody know who has these at a better price than the normal places like Spruce? >Thanks, > >Paul ________________________________________________________________________________
From: "Tom & Cathy Ervin" <tcervin(at)valkyrie.net>
Subject: Oil Cooler Block Fittings
Date: May 01, 2005
List, Mounting a S&W 8432R oil cooler to the left side firewall of my RV6-A, new 360-A1A and would like input on the following: 1) Do I need to purchase fittings to go in the block oil inlet and outlets after the plugs are removed or do the oil hoses screw directly in the block? 2) If fittings are required which ones and what is a good source to acquire them from? I have a 3 in. cooling hose running off the left baffle with a door to a cooler which is sized for a 0-540! Been told oil temps should not be a problem. All input appreciated. Tom in Ohio ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Long glide to landing
Date: May 01, 2005
----- Original Message ----- From: "Tracy Crook" <lors01(at)msn.com> Subject: Re: RV-List: Long glide to landing > > I agree that this is good practice. I did find that the glide ratio > varied greatly depending on idle speed of engine not to mention engine > stopped. I was surprised that my engine out (fixed pitch prop stopped) > sink rate was higher than with even a low idle. I'd always heard that it > was the other way around. > > How were you guys testing? > > Tracy Crook > Rotary powered RV-4 > Charles Heathco wrote: Tracy and others... Most fixed pitch RV's get a meaningful amount of thrust at idle, up to a speed that equals the advance rate of the prop x RPM. That math is boring, but here's a real-world example that might shed some light: A simple For instance, my airplane trues out at 200 mph at 2700 rpm and at 1000' or less. Dividing that RPM by 4 gives 675 rpm, and dividing the speed by 4 gives 50 mph. So, at 675 RPM, the prop will be giving some amount of thrust up to 50 mph, beyond that, it is a drag producer. However, in an idle throttle glide, my airplane idles at something like 1150 rpm at 80 miles an hour. If you ratio the RPM vs speed between glide and ground idle, you get 1150rpm /675rpm = (X mph)/50mph. Solve for X and you get 85 mph. So, my prop is more or less thrust neutral at 85 mph in a glide, and is probably adding a little thrust below that speed. That creates one of the minor challenges of landing a fixed pitch prop RV - once you flare, the residual prop thrust adds a meaningful amount of distance as you float down the runway in ground effect. All of which wraps around to your observation that that a fixed pitch RV doesn't glide as well with the prop stopped as with the engine at idle. KB ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Long glide to landing
Date: May 01, 2005
----- Original Message ----- From: "Tracy Crook" <lors01(at)msn.com> Subject: Re: RV-List: Long glide to landing > > I agree that this is good practice. I did find that the glide ratio > varied greatly depending on idle speed of engine not to mention engine > stopped. I was surprised that my engine out (fixed pitch prop stopped) > sink rate was higher than with even a low idle. I'd always heard that it > was the other way around. > > How were you guys testing? > > Tracy Crook > Rotary powered RV-4 > Charles Heathco wrote: Tracy and others... Most fixed pitch RV's get a meaningful amount of thrust at idle, up to a speed that equals the advance rate of the prop x RPM. That math is boring, but here's a real-world example that might shed some light: A simple For instance, my airplane trues out at 200 mph at 2700 rpm and at 1000' or less. Dividing that RPM by 4 gives 675 rpm, and dividing the speed by 4 gives 50 mph. So, at 675 RPM, the prop will be giving some amount of thrust up to 50 mph, beyond that, it is a drag producer. However, in an idle throttle glide, my airplane idles at something like 1150 rpm at 80 miles an hour. If you ratio the RPM vs speed between glide and ground idle, you get 1150rpm /675rpm = (X mph)/50mph. Solve for X and you get 85 mph. So, my prop is more or less thrust neutral at 85 mph in a glide, and is probably adding a little thrust below that speed. That creates one of the minor challenges of landing a fixed pitch prop RV - once you flare, the residual prop thrust adds a meaningful amount of distance as you float down the runway in ground effect. All of which wraps around to your observation that that a fixed pitch RV doesn't glide as well with the prop stopped as with the engine at idle. KB ________________________________________________________________________________
Date: May 01, 2005
From: Tedd McHenry <tedd(at)vansairforce.org>
Subject: Re: Long glide to landing
Here's how we used to set up forced landings in the Canadian air force. Start by knowing how much altitude you lose in a comfortable 360-degree turn. We used 30 degrees of bank, but you can use whatever bank angle feels most comfortable at best-glide speed. Add a little to that for a margin of error (we added 500 feet for training jets, but less would probably be appropriate for an RV). That number is the altitude for high key, the starting point of the forced landing. Ideally, in a forced landing situation, you arrive over the button of the runwat at high key, execute a 360 turn, and land. Once you know high key, it's easy to calculate what low key (the 180-degree point) and final key (the 270-degree point) should be. Inevitabley, you'll find yourself arriving at the runway above or below high key altitude. If it looks like you're going to be a bit above high key, then S-turn or slip to kill the extra altitude. If you still arrive at high key a bit high, then fly an oval pattern instead of a 360-degree turn. For example, if you arrive at high key 500 feet high, then do a 180-degree turn followed by a short downwind leg (losing about 250 feet, plus or minus a bit depending on wind) followed by a final turn to the runway. If you arrivce at double the high key altitude, simply do two 360-degree turns. If it looks like you're going to arrive below high key altitude you need to modify the approach. In a real-world situation you're unlikely to be approaching from the extended runway centerline. So you'll be joining the 360-degree pattern at a tangent point. Imagine that the pattern is a giant roll of tape, with the free end over the button of the runway. In your mind's eye, unwind the tape until it's coincident with your approach path. That gives you a de facto "high key" at some point along your track. Aim to arrive over that point at high key altitude. If you practice forced landings that way (which, admittedly, requires access to an airfield with very little traffic), you'll find that you can do them very reliably, with as much confidence as a glider pilot has on any normal landing. Tedd McHenry Surrey, BC, Canada ________________________________________________________________________________
Date: May 01, 2005
From: Chris W <1qazxsw23edcvfr45tgbnhy67ujm(at)cox.net>
Subject: Re: Long glide to landing
Tracy Crook wrote: > >I agree that this is good practice. I did find that the glide ratio varied greatly depending on idle speed of engine not to mention engine stopped. I was surprised that my engine out (fixed pitch prop stopped) sink rate was higher than with even a low idle. I'd always heard that it was the other way around. > >How were you guys testing? > > I recently did some testing in the RV7 for FS 2004 just for fun. I started at 10,000 ft which was 8,800 ft AGL. First I killed the engine, glided down and landed in a field with the prop windmilling. The glide lasted 14 nautical miles that time. The second time I stopped the prop. The trick to that in the simulator, is you have to pull the nose up to about 60 degrees, wait for it to fall and then recover. A full flaps stall will not stop the prop in the simulator. That time I made it 19 nautical miles. Both times I held 95 +/- 3 knots. I have not tried it with the engine at idle. Just for the record, the simulated RV7 has a 200hp IO360 with 2 blade constant speed prop at the time of the 2 glides there were about 35 gallons of fuel, a 170lbs pilot and 170 lbs passenger. I was curious if this comes close to any real RV7s out there. If someone wants me to try a different scenario to compare to something they did, let me know. I did do one test to compare idle with engine out windmilling, I was flying a WOT about 5 feet off the ground heading toward a 3 mile runway (Edwards Air Force Base). As soon as I crossed the runway threshold, I either killed the engine or took it to idle. The idle took me almost exactly the full 3 miles of the runway before I had to touchdown. With the engine out, it went about 2 miles before touch down. No flaps either time of course. -- Chris W ________________________________________________________________________________
From: "DAVID REEL" <dreel(at)cox.net>
Subject: Lower cowl movement estimate
Date: May 01, 2005
Does anybody have an estimate for how far up the lower cowl on an RV8A would move in flight? I have the epoxy honeycomb sandwich type cowl shipped about 5 years ago. I'm wondering how much alternator pulley clearance I need to provide & why we don't align our filtered air box and cowl air inlets with the cowl displaced upwards. Upon researching the archives, engine sag when pulling G's rather than cowl movement due to aerodynamic pressure may be the problem. But the need is still the same. Virtually nobody gives actual clearances static or otherwise, nor do they mention the direction of movement. I know that many have experienced alternator pulley contact problems & feel whatever hard numbers or even estimated numbers anyone could provide would be very helpful. Imagine if someone noted that they had 1/4" vertical clearance & experienced chafing, increased it to 3/4" & had no further problem. Even a few people reporting how much clearance they had & that there was no problem would be great. Next time your top cowl is off, how about sticking a drill or a small piece of wood in between whatever is closest and your cowl & let us all know your actual clearance & whether there has been contact? Dave Reel - RV8A ________________________________________________________________________________
From: "dave" <dford(at)michweb.net>
Subject: compression checking an engine
Date: May 01, 2005
I'd like to check compressions on my engine and since I currently don't know how to do that, wondering if someone could forward a link or instructions regarding tools and procedure for doing that. Dave Ford RV6 ________________________________________________________________________________
From: "RV3 PILOT" <RMCKEE(at)mn.rr.com>
Subject: Tip up Canopy Vs. Slider
Date: May 01, 2005
0.38 FROM_NO_LOWER From address has no lower-case characters I would like to know if the tip up canopies seal better than the sliders do around the fuselage sides? I have heard that the sliders leak a fair amount of air around the sides of the canopy in flight. If anyone can help me out with this please e-mail me. Robin RV3B Kit 11356 Minnesota RMCKEE(at)MN.RR.COM ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: Tip up Canopy Vs. Slider
Date: May 01, 2005
Robin, The tip up comes down on the side rails and have a "P" channel running the length of the each side of the canopy. I find it really seals quite effectively. Never flown in a slider, so don't know how the two compare. Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC 28104 ----- Original Message ----- From: "RV3 PILOT" <RMCKEE(at)mn.rr.com> Subject: RV-List: Tip up Canopy Vs. Slider > > I would like to know if the tip up canopies seal better than the sliders > do around the fuselage sides? I have heard that the sliders leak a fair > amount of air around the sides of the canopy in flight. If anyone can > help me out with this please e-mail me. > > Robin > RV3B Kit 11356 > Minnesota > RMCKEE(at)MN.RR.COM > > > ________________________________________________________________________________
From: "LARRY ADAMSON" <rvhi03(at)msn.com>
Subject: Re: Long glide to landing
Date: May 01, 2005
----- Original Message ----- From: Chris W Subject: Re: RV-List: Long glide to landing Something that the simulated RV doesn't do to well, is the braking effect of the C/S prop in fine pitch. It's more like approaching with a fixed pitch. How this will effect the rest of the simulated scenario, I have no idea. < The trick to that in the simulator, is you have to pull the nose From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: compression checking an engine
Date: May 01, 2005
AV 43-13.1B has a section on differential compression checking. Cy Galley - Chair, AirVenture Emergency Aircraft Repair A Service Project of Chapter 75 EAA Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: "dave" <dford(at)michweb.net> Subject: RV-List: compression checking an engine > > I'd like to check compressions on my engine and since I currently don't > know how to do that, wondering if someone could forward a link or > instructions regarding tools and procedure for doing that. > > Dave Ford > RV6 > > > ________________________________________________________________________________
From: "Aircraft Technical Book Company" <winterland(at)rkymtnhi.com>
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 01, 2005
I made this suggestion once before. There was little interest, but it might be worth suggesting again. . It would be a good thing for everyone to actually try a couple real engine off landings in their own plane. See for yourself what happens when the fan stops. But do it in a safe way with lots of room and lots of options. So lets all have a summer fly-in at some huge, empty, ex-military airport in the middle of the plains. Someplace with no obstructions, no traffic, and no-brainer approaches. A place we can, one at a time, set up a couple thousand feet over the runway and pull out the mixture - all the way. If enough of us were interested we can bring in some instructors, perhaps from Vans. And then once we're more comfortable, perhaps have spot landing constests with some real nice prizes. For sure we'd all have a lot of fun and it would make better and safer pilots of everyone. Let me know if you're interested. If a couple dozen people say they are, I'll help set it up. Andy Builder's Bookstore 970 887-2207 www.buildersbooks.com ________________________________________________________________________________
Date: May 01, 2005
From: Tedd McHenry <tedd(at)vansairforce.org>
Subject: Langley (BC) Fly-in 2005
Just a reminder that the Langley, BC fly-in is Saturday, June 4, 2005. This is the annual fly-in of the Western Canada Wing. Langley, BC, is about 20 nm north of Bellingham, WA. We generally have a good turnout of RVs from all over BC, and a good contingent from the U.S., too. Details are on our web page, http://www.vansairforce.org/CYNJ/ For U.S. visitors, the Home Wing web page has all the information you need on border crossing procedures. http://www.edt.com/homewing/international/ I hope to see lots of RV-Listers there. --- Tedd McHenry Van's Air Force Western Canada Wing www.vansairforce.org tedd(at)vansairforce.org ________________________________________________________________________________
From: "Fabian Lefler" <fablef(at)bellsouth.net>
Subject: Re: Aluminum Air Vents
Date: May 01, 2005
Stein, ... and maybe some people shouldn't be knocking other people's products without having all of the information. Two years ago, I sold the Airkit vents, however, I decided to start making them myself to duplicate Van's size and improve in some other areas. Additionally, my vents are much cheaper. Airkits are $298.0 a pair, and mine are $225/pair for the black ones and $245/air for the clear ones. What $5.00 dollars difference are you talking about? In the future, sitck to what you know best and let others do their thing. For those who want to see a photo of the vents, here it is: http://www.affordablepanels.com/aluminum_vents_files/IM001220.JPG Fabian ----- Original Message ----- From: "Stein Bruch" <stein(at)steinair.com> Subject: RE: RV-List: Aluminum Air Vents > > Ummm....not really - Sometimes people take credit for things that they > shouldn't.... > > Anyway, these vents are actually made by a company called "Airkit, LLC". > The same Vents are sold for the same price by a lot of people, including > Van's Aircraft > (http://www.vansaircraft.com/cgi-bin/catalog.cgi?ident=1114912044-64-423&bro > wse=heatvent). I actually looked into stocking them, but with such a small > company like Airkit and not a lot of margin, I figured I'd just point people > to the companies website (http://www.airkitllc.com) and tell people to buy > them direct for only $5.00 more. I like to see small business like that > succeed so I throw as much business directly to them as I can! > > Those are nice vents but pretty large. I use the standard sized Wemac > Aluminum vents in both my RV's and like them the best. I've used the large > ones, but IHMO, they aren't quite as nice overall as the smaller ones when > it comes to directing airflow. I like to direct a stream of air onto my > face, chest or forehead when I like, and the smaller 1.5+" ones work best > for me. You can get them for $50+ something at ACS or other places, but my > personal favorite place is just digging through an aircraft junkyard (like > Wentworth) until you find some you need. They usually sell them for much > less. > > Just my 2 cents as usual! > > Cheers, > Stein. > > P.S., no flames intended. > > -----Original Message----- > From: owner-rv-list-server(at)matronics.com > [mailto:owner-rv-list-server(at)matronics.com]On Behalf Of Charlie Kuss > To: rv-list(at)matronics.com > Subject: Re: RV-List: Aluminum Air Vents > > > Paul > Local RV-9A builder Fabian Lefler owns AFFORDABLE PANELS.com Fabian > designed and is marketing a very nice aluminum vent the same size as Vans. > His price is better than most of the other aluminum vents I've seen. See > > http://www.affordablepanels.com/aluminum_vents.htm > > Charlie Kuss > > > > > >I don't particularly like the plastic eyeball vents that Vans supplies and > >would like to use aluminum vents instead. I recall seeing several units > >advertised but can't seem to remember where. Does anybody know who has > >these at a better price than the normal places like Spruce? > > > >Thanks, > > > >Paul > >RV-8 > > > > > > ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: May 01, 2005
Subject: Re: Hinge pin on fiberglass 6a gear
In a message dated 05/01/2005 1:33:48 PM Central Standard Time, don(at)dmack.net writes: They are Rocket fiberglass fairings. Since they are on a 6A they will be under the wing. How do I install the hinge pin? >>> Hi Don- I also used the Rocket fairings on my 6A and the pins can easily be inserted from the bottom- install the pin before you attach the upper ends of the fairings as you can rotate the fairing (outboard at the rear) to get a better angle to shove the pin in. You are using the smaller hinges (don't have the # or size handy, but smaller than the cowl halves) with the thin pins? They flex quite easily. I've never seen any split in the middle... Mark Phillips ________________________________________________________________________________
From: "dave" <dford(at)michweb.net>
Subject: high egts
Date: May 01, 2005
I am having high egts and chts at different times on my #2 cylinder relative to other cylinders. Even at an idle #2 can be 200 deg higher than the rest, is into yellow during climb, getting into red at 1500 deg. Sometimes during a decent it will go above 1450 when all other cylinders are in 1200s. #2 is also my hottest cht though usually in the green below 400deg. I have changed injectors between 1 and 2 with no change, have heard to check air tube into lower case but don't know about that one--could intake valve be leaking? Have yet to confirm egt probe. Any suggestions? Dave Ford RV6 ________________________________________________________________________________
Date: May 01, 2005
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: high egts
dave wrote: > >I am having high egts and chts at different times on my #2 cylinder relative to other cylinders. Even at an idle #2 can be 200 deg higher than the rest, is into yellow during climb, getting into red at 1500 deg. Sometimes during a decent it will go above 1450 when all other cylinders are in 1200s. #2 is also my hottest cht though usually in the green below 400deg. >I have changed injectors between 1 and 2 with no change, have heard to check air tube into lower case but don't know about that one--could intake valve be leaking? Have yet to confirm egt probe. Any suggestions? > >Dave Ford >RV6 > Don't know about high cht's (didn't have multiprobe cht) but I had intermittant rough running & found a stubb intake tube loose in the oil pan. (love that aircraft quality) Charlie ________________________________________________________________________________
From: Vanremog(at)aol.com
Date: May 01, 2005
Subject: Re: Tip up Canopy Vs. Slider
In a message dated 5/1/2005 1:14:41 P.M. Pacific Daylight Time, RMCKEE(at)mn.rr.com writes: I would like to know if the tip up canopies seal better than the sliders do around the fuselage sides? I have heard that the sliders leak a fair amount of air around the sides of the canopy in flight. If anyone can help me out with this please e-mail me. ======================================== If you block up the slider during fitting and assembly of the aft skirts, they will then fit quite nice and snug when you remove the blocks. The only air/rain we have that leaks into the slider is the very tiny bit that comes in around the sliding rail cap at the top due to the low pressure in this area. One of these days I'll fashion a way to plug this area. IMO the slider is a pretty tight fit if done well. GV (RV-6A N1GV O-360-A1A, C/S, Flying 742hrs, Silicon Valley, CA) ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)petroblend.com>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 01, 2005
I was giving a BFR this week and I asked the pilot what the rate of decent was power off in his airplane. He said, "I don't know, I suppose around 500 fpm." I said we would go up over the airport and pull the mixture and find out. He was concerned about that. I asked him why? He said "What if it doesn't restart?" We land, I replied. If anyone is concerned in the least about an engine failure at 3000 AGL directly over a 6500 x 250 ft runway they should not be flying single engine airplanes. We pulled the mixture and flew best glide speed and the airplane came down 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. We found that 1/3 flaps and idle thrust simlated that decent, then we practiced deadstick overhead 360 and 180 approaches to a specific point on the runway, without going short. He did well and I would suspect his chances of successfully making a deadstick landing increased dramatically. If you are not comfortable shutting down your engine over an airport, find a flight instructor and go do it ASAP. Unfortunately most flight instructors are teaching to gain experience rather than share it. If your flight instructor is unwilling to do it, find a different flight instructor. A successful outcome from a bad situation is directly related to the confidence the pilot has in that outcome. If you have realistically trained for, and successfully completed deadstick landings on a point, you will have a much higher level of confidence in the outcome and that increases the likelyhood of a successful outcome WHEN (not if) the fire goes out. Tailwinds, Doug Rozendaal ________________________________________________________________________________
Date: May 01, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Did you stop the propellor when you pulled the mixture, or was it still windmilling? If the propellor was still windmilling, then you may not have simulated a realistic condition. A windmilling propellor creates as much drag as a flat plate the diameter of your propellor... If you stop the prop, the drag on your aircraft will decrease significantly, and your descent rate will decrease as well. -Rob Doug Rozendaal wrote: > > I was giving a BFR this week and I asked the pilot what the rate of decent > was power off in his airplane. He said, "I don't know, I suppose around 500 > fpm." I said we would go up over the airport and pull the mixture and find > out. He was concerned about that. I asked him why? He said "What if it > doesn't restart?" We land, I replied. > We pulled the mixture and flew best glide speed and the airplane came down > 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. We > found that 1/3 flaps and idle thrust simlated that decent, then we practiced > deadstick overhead 360 and 180 approaches to a specific point on the runway, > without going short. He did well and I would suspect his chances of > successfully making a deadstick landing increased dramatically. ________________________________________________________________________________
From: "Curt Reimer" <cgreimer(at)mts.net>
Subject: Re: Long glide to landing
Date: May 01, 2005
In flight testing my RV-6, I did some glide tests at various airspeeds and plotted the results. I show a maximum glide ratio of 10.4 with the engine idling and 8.7 with the engine off, prop windmilling. That was at a mean altitude of 4000 feet and 84 knots indicated in both cases. I have a fixed pitch wood "climb" prop. I have stopped the prop in a glide, by slowing to <60 knots, but I haven't measuring the glide characteristics in that condition. Stopping the prop - and keeping it from spinning up again - is a rather distracting procedure and in a real engine-out situation I'd probably be far too busy to bother with all that unless I had a lot of altitude/time to spare. With it's slightly higher aspect ratio, I'd expect an RV-7 to do a bit better than a -6 but in the same ballpark. Curt > I recently did some testing in the RV7 for FS 2004 just for fun. I > started at 10,000 ft which was 8,800 ft AGL. First I killed the engine, > glided down and landed in a field with the prop windmilling. The glide > lasted 14 nautical miles that time. The second time I stopped the > prop. The trick to that in the simulator, is you have to pull the nose > up to about 60 degrees, wait for it to fall and then recover. A full > flaps stall will not stop the prop in the simulator. That time I made > it 19 nautical miles. Both times I held 95 +/- 3 knots. I have not > tried it with the engine at idle. Just for the record, the simulated > RV7 has a 200hp IO360 with 2 blade constant speed prop at the time of > the 2 glides there were about 35 gallons of fuel, a 170lbs pilot and 170 > lbs passenger. I was curious if this comes close to any real RV7s out > there. If someone wants me to try a different scenario to compare to > something they did, let me know. I did do one test to compare idle with > engine out windmilling, I was flying a WOT about 5 feet off the ground > heading toward a 3 mile runway (Edwards Air Force Base). As soon as I > crossed the runway threshold, I either killed the engine or took it to > idle. The idle took me almost exactly the full 3 miles of the runway > before I had to touchdown. With the engine out, it went about 2 miles > before touch down. No flaps either time of course. > > -- > Chris W ________________________________________________________________________________
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
From: "Greg Young" <gyoung@cs-sol.com>
I beg to differ - windmilling IS the realistic condition. If the power stops either because of lack of fuel or ignition and the prop keeps windmilling at glide speed then that's what you should simulate/practice. At low altitude you have to take what you get. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A > > Did you stop the propellor when you pulled the mixture, or > was it still windmilling? If the propellor was still > windmilling, then you may not have simulated a realistic condition. > > A windmilling propellor creates as much drag as a flat plate > the diameter of your propellor... If you stop the prop, the > drag on your aircraft will decrease significantly, and your > descent rate will decrease as well. > > -Rob > ________________________________________________________________________________
From: HCRV6(at)aol.com
Date: May 02, 2005
Subject: Re: try-it-yourself fly-in - was Long glide to landing
In a message dated 5/1/05 3:58:31 PM Pacific Daylight Time, winterland(at)rkymtnhi.com writes: > Let me know if you're interested. If a couple dozen people say they are, > I'll help set it up. > > Andy: Sounds like a good idea. You can count me in except for the > last two weeks of July and the first week in August ( shouldn't be a problem > since those dates coincide with Oshkosh). > > Harry Crosby > RV-6 N16CX, 69 hours ________________________________________________________________________________
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
From: "Greg Young" <gyoung@cs-sol.com>
I beg to differ - windmilling IS the realistic condition. If the power stops either because of lack of fuel or ignition and the prop keeps windmilling at glide speed then that's what you should simulate/practice. At low altitude you have to take what you get. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A > > Did you stop the propellor when you pulled the mixture, or > was it still windmilling? If the propellor was still > windmilling, then you may not have simulated a realistic condition. > > A windmilling propellor creates as much drag as a flat plate > the diameter of your propellor... If you stop the prop, the > drag on your aircraft will decrease significantly, and your > descent rate will decrease as well. > > -Rob > ________________________________________________________________________________
From: "Garth Shearing" <Garth(at)islandnet.com>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 01, 2005
And I beg to differ with you, Greg. If you want minimum sink rate, low drag, and maximum distance to glide, you have to reduce speed to stop the prop, and then increase speed to best glide ratio. In the unlikely event that the best glide ratio speed restarts the windmilling, then use a slightly lower glide speed. In an engine out emergency, that is the realistic and best condition. Don't ask me how I know. Garth Shearing VariEze & 90% RV6A Victoria BC Canada ----- Original Message ----- From: "Greg Young" <gyoung@cs-sol.com> Subject: RE: RV-List: try-it-yourself fly-in - was Long glide to landing > > I beg to differ - windmilling IS the realistic condition. If the power > stops either because of lack of fuel or ignition and the prop keeps > windmilling at glide speed then that's what you should > simulate/practice. At low altitude you have to take what you get. > > Regards, > Greg Young - Houston (DWH) > RV-6 N6GY - project Phoenix > Navion N5221K - just an XXL RV-6A > > >> >> Did you stop the propellor when you pulled the mixture, or >> was it still windmilling? If the propellor was still >> windmilling, then you may not have simulated a realistic condition. >> >> A windmilling propellor creates as much drag as a flat plate >> the diameter of your propellor... If you stop the prop, the >> drag on your aircraft will decrease significantly, and your >> descent rate will decrease as well. >> >> -Rob ________________________________________________________________________________
From: owner-rv-list-server(at)matronics.com
Subject: Lower cowl movement estimate
Date: May 02, 2005
I'd think the thing to do is go look at the cowls of similar aerobatic airplanes and measure the gap - CAP 10, any other airplane which has an IO360 + CS + dynafocal 1. I have access to a CAP 10 (C/S excepted) and shall report what I find. Michle > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of DAVID REEL > Sent: Sunday, May 01, 2005 8:15 PM > To: rvlist > Subject: RV-List: Lower cowl movement estimate > > > Does anybody have an estimate for how far up the lower cowl on an RV8A > would move in flight? I have the epoxy honeycomb sandwich type cowl > shipped about 5 years ago. I'm wondering how much alternator pulley > clearance I need to provide & why we don't align our filtered air box and > cowl air inlets with the cowl displaced upwards. > > Upon researching the archives, engine sag when pulling G's rather than > cowl movement due to aerodynamic pressure may be the problem. But the > need is still the same. Virtually nobody gives actual clearances static > or otherwise, nor do they mention the direction of movement. I know that > many have experienced alternator pulley contact problems & feel whatever > hard numbers or even estimated numbers anyone could provide would be very > helpful. Imagine if someone noted that they had 1/4" vertical clearance & > experienced chafing, increased it to 3/4" & had no further problem. Even > a few people reporting how much clearance they had & that there was no > problem would be great. Next time your top cowl is off, how about > sticking a drill or a small piece of wood in between whatever is closest > and your cowl & let us all know your actual clearance & whether there has > been contact? > > Dave Reel - RV8A > > > > > ________________________________________________________________________________
From: "Ed Anderson" <eanderson(at)carolina.rr.com>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
Excellent advice, Doug Having made two dead stick landings and one partial power landing, I can vouch that even a small amount of practice can change an engine-out event from an almost mind-numbing experience to one of heighten concentration and awareness. I haven't had to replace the seat cushion since the first one. Although I understand that power-on landings is becoming the "recommended" best way of landing an RV, I still make every landing from the pattern an "engine-out" approach - its good practice in my opinion. The RV is not a glider, but it really does not become a brick either if you pay attention to your airspeed. The 10:1 glide ratio advertise is fairly close to what I have experienced with a stopped prop. But, you really need to know your best air speeds for max distance and minimum altitude lost BEFORE it happens. Ed Anderson ----- Original Message ----- From: "Doug Rozendaal" <dougr(at)petroblend.com> Subject: Re: RV-List: try-it-yourself fly-in - was Long glide to landing > > I was giving a BFR this week and I asked the pilot what the rate of decent > was power off in his airplane. He said, "I don't know, I suppose around > 500 > fpm." I said we would go up over the airport and pull the mixture and > find > out. He was concerned about that. I asked him why? He said "What if it > doesn't restart?" We land, I replied. > > If anyone is concerned in the least about an engine failure at 3000 AGL > directly over a 6500 x 250 ft runway they should not be flying single > engine > airplanes. > > We pulled the mixture and flew best glide speed and the airplane came down > 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. > We > found that 1/3 flaps and idle thrust simlated that decent, then we > practiced > deadstick overhead 360 and 180 approaches to a specific point on the > runway, > without going short. He did well and I would suspect his chances of > successfully making a deadstick landing increased dramatically. > > If you are not comfortable shutting down your engine over an airport, find > a > flight instructor and go do it ASAP. > > Unfortunately most flight instructors are teaching to gain experience > rather > than share it. If your flight instructor is unwilling to do it, find a > different flight instructor. > > A successful outcome from a bad situation is directly related to the > confidence the pilot has in that outcome. If you have realistically > trained > for, and successfully completed deadstick landings on a point, you will > have > a much higher level of confidence in the outcome and that increases the > likelyhood of a successful outcome WHEN (not if) the fire goes out. > > Tailwinds, > Doug Rozendaal > > > ________________________________________________________________________________
From: "Mike Robertson" <mrobert569(at)hotmail.com>
Subject: compression checking an engine
Date: May 02, 2005
Dave, If you buy a compression tester from ACS or one of the other fine retail outlets, there are instructions included with each one. Basically, you bring the cylinder you are testing to top dead center, connect the tester, and apply 80 ps to the cylinder (keeping a good hold on the prop). The one gauge on the tester will show you the 80 psi and the other will show you the cylinder pressure. Thats it! Mike Robertson >From: "dave" <dford(at)michweb.net> >Reply-To: rv-list(at)matronics.com >To: >Subject: RV-List: compression checking an engine >Date: Sun, 1 May 2005 14:34:16 -0500 > > >I'd like to check compressions on my engine and since I currently don't >know how to do that, wondering if someone could forward a link or >instructions regarding tools and procedure for doing that. > >Dave Ford >RV6 > > ________________________________________________________________________________
From: "Vic Jacko" <vicwj(at)earthlink.net>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
Just one more thought to unfuel the fire (pun intended) If you want to extend your glide with a windmilling prop then keep the throttle wide open (assuming it is not running) to reduce the pumping losses. If you pull the mixture to full lean the throttle can be opened all the way. If you were to test the difference between closed throttle or wide open I think you will find open is better. Otherwise with the prop turning you have a big air compressor sucking at the throttle plate with it closed. IMHO! Vic ----- Original Message ----- From: "Rob Prior (rv7)" <rv7(at)b4.ca> Subject: Re: RV-List: try-it-yourself fly-in - was Long glide to landing > > Did you stop the propellor when you pulled the mixture, or was it still > windmilling? If the propellor was still windmilling, then you may not > have simulated a realistic condition. > > A windmilling propellor creates as much drag as a flat plate the > diameter of your propellor... If you stop the prop, the drag on your > aircraft will decrease significantly, and your descent rate will > decrease as well. > > -Rob > > Doug Rozendaal wrote: >> >> I was giving a BFR this week and I asked the pilot what the rate of >> decent >> was power off in his airplane. He said, "I don't know, I suppose around >> 500 >> fpm." I said we would go up over the airport and pull the mixture and >> find >> out. He was concerned about that. I asked him why? He said "What if it >> doesn't restart?" We land, I replied. > >> We pulled the mixture and flew best glide speed and the airplane came >> down >> 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. >> We >> found that 1/3 flaps and idle thrust simlated that decent, then we >> practiced >> deadstick overhead 360 and 180 approaches to a specific point on the >> runway, >> without going short. He did well and I would suspect his chances of >> successfully making a deadstick landing increased dramatically. > > > ________________________________________________________________________________
Date: May 02, 2005
From: Mark Schrimmer <mschrimmer(at)pacbell.net>
Subject: Elastic Insert platenuts
Does anybody know what elastic insert platenuts are used for? Do they work better than than the all-metal nuts provided with the kits? Thanks, Mark ________________________________________________________________________________
From: "Jeff Dowling" <shempdowling2(at)earthlink.net>
Subject: Re: Long glide to landing
Date: May 02, 2005
3 questions. 1. I remember reading something about shutting your engine down a certain way to prevent damage when practicing engine out. What is it? 2. How do you prevent shock cooling? It sure seems like it would take a while at 5000' for it to cool enough before shutting down but I guess thats what you do. 3. Whats a typical glide ratio for a constant speed prop? I doubt there's much difference between models. Shemp/Jeff Dowling RV-6A, N915JD 190 hours Chicago/Louisville ----- Original Message ----- From: "Curt Reimer" <cgreimer(at)mts.net> Subject: Re: RV-List: Long glide to landing > > In flight testing my RV-6, I did some glide tests at various airspeeds and > plotted the results. I show a maximum glide ratio of 10.4 with the engine > idling and 8.7 with the engine off, prop windmilling. That was at a mean > altitude of 4000 feet and 84 knots indicated in both cases. I have a fixed > pitch wood "climb" prop. > > I have stopped the prop in a glide, by slowing to <60 knots, but I haven't > measuring the glide characteristics in that condition. Stopping the prop - > and keeping it from spinning up again - is a rather distracting procedure > and in a real engine-out situation I'd probably be far too busy to bother > with all that unless I had a lot of altitude/time to spare. > > With it's slightly higher aspect ratio, I'd expect an RV-7 to do a bit > better than a -6 but in the same ballpark. > > Curt > > >> I recently did some testing in the RV7 for FS 2004 just for fun. I >> started at 10,000 ft which was 8,800 ft AGL. First I killed the engine, >> glided down and landed in a field with the prop windmilling. The glide >> lasted 14 nautical miles that time. The second time I stopped the >> prop. The trick to that in the simulator, is you have to pull the nose >> up to about 60 degrees, wait for it to fall and then recover. A full >> flaps stall will not stop the prop in the simulator. That time I made >> it 19 nautical miles. Both times I held 95 +/- 3 knots. I have not >> tried it with the engine at idle. Just for the record, the simulated >> RV7 has a 200hp IO360 with 2 blade constant speed prop at the time of >> the 2 glides there were about 35 gallons of fuel, a 170lbs pilot and 170 >> lbs passenger. I was curious if this comes close to any real RV7s out >> there. If someone wants me to try a different scenario to compare to >> something they did, let me know. I did do one test to compare idle with >> engine out windmilling, I was flying a WOT about 5 feet off the ground >> heading toward a 3 mile runway (Edwards Air Force Base). As soon as I >> crossed the runway threshold, I either killed the engine or took it to >> idle. The idle took me almost exactly the full 3 miles of the runway >> before I had to touchdown. With the engine out, it went about 2 miles >> before touch down. No flaps either time of course. >> >> -- >> Chris W > > > ________________________________________________________________________________
From: "Jeff Dowling" <shempdowling2(at)earthlink.net>
Subject: Re: compression checking an engine
Date: May 02, 2005
Its a 2 man job. 80 psi is tough to hold if the prop gets off tdc. Shemp/Jeff Dowling RV-6A, N915JD 190 hours Chicago/Louisville ----- Original Message ----- From: "Mike Robertson" <mrobert569(at)hotmail.com> Subject: RE: RV-List: compression checking an engine > > Dave, > > If you buy a compression tester from ACS or one of the other fine retail > outlets, there are instructions included with each one. Basically, you > bring the cylinder you are testing to top dead center, connect the tester, > and apply 80 ps to the cylinder (keeping a good hold on the prop). The > one > gauge on the tester will show you the 80 psi and the other will show you > the > cylinder pressure. Thats it! > > Mike Robertson > >>From: "dave" <dford(at)michweb.net> >>Reply-To: rv-list(at)matronics.com >>To: >>Subject: RV-List: compression checking an engine >>Date: Sun, 1 May 2005 14:34:16 -0500 >> >> >>I'd like to check compressions on my engine and since I currently don't >>know how to do that, wondering if someone could forward a link or >>instructions regarding tools and procedure for doing that. >> >>Dave Ford >>RV6 >> >> > > > ________________________________________________________________________________
From: "Larry Pardue" <n5lp(at)warpdriveonline.com>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
> >I think it would be a great exercise to see > just how easy/hard it is to stop the prop ..... and keep it stopped > ..... and then see what the real-world differences there are. When I fiddled around with this on my airplane I found it took about 120 knots to start the prop turning. http://www.matronics.com/searching/getmsg_script.cgi?INDEX=124394593?KEYS=larry_pardue?LISTNAME=RV?HITNUMBER=180?SERIAL=08295813183?SHOWBUTTONS=YES The speed to stop the prop seemed to vary from 60 to 70 knots depending on engine temperature. Larry Pardue Carlsbad, NM RV-6 N441LP Flying http://n5lp.net ________________________________________________________________________________
Date: May 02, 2005
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Long glide to landing
The effort and experimentation in glide ratio flight test is excellent, but how will that work in an emergency. Tedd nice explanation of hi-key/ 360 overhead approach. I guess what is important to me is how can I use this info in a real engine failure scenario. "100 and 1.4" (speed 100mph and 1.4 kt mile/per thousand altitude- or 600 ft/ NM) So my first job after an engine failure/ loss of power would be get to best glide speed (initial target speed 100mph than adjust for weight, wind). Trim to that, while simultaneously trouble shooting engine (boost pump, switch tanks, mixture, carb heat, ignition etc... as required) and look for a landing spot within 1.4 kt miles per thousand feet agl. Fly the airplane. From what I got from all this that an RV will glide somewhere *10.5 to 1 thru 8.7 to 1 ratio (*idle power). (Realistic engine out glide will be closer to the 8.7 to 1. Numbers above 9 or 10 seem to be affected by partial idle power or tail winds. A real light RV flown perfectly could do better than 8.7 to 1 but again I am looking for something conservative I can remember and use in an emergency, with a little margin for less than perfect speed control.) Also I got best glide (max distance) is some where in the 81kt - 95 kt range (varies with weight, altitude and head wind). Therefore I remember 100mph (bigger mark on a/s indicator) and adjust as needed for weight. Typical glide speed for RV best glide 84 kts = 96 mph. Min sink is under slower. Assuming engine is ka-put and I am making an emergency engine-out glide/landing, I would assume glide ratio closer to 8. 7 to 1 than 10.5 to 1, which sounds a little high. Therefore for every 1000 ft altitude I can glide 1.4 kt miles (sink approx 950 ft/min or 600 ft/NM). As far as windmilling prop or not, I assume the worst case, windmilling. The most critical condition is when you have little altitude, so I would not personally mess with trying to stop the prop. If I was at 12,000 agl and had time I might consider it, but I would try to get the engine running at first and keep the prop windmilling. I can't recall ever seeing this in a POH or in training. If you think you would attempt or consider trying to stop the prop (windmilling) in a real emergency, I would suggest you practice it first under controlled conditions. I have not, from what I hear is it takes near stall speed and may be even a touch of flaps? In the time messing with all that, how much altitude do you loose vs. just going to best glide and time lost making headway towards your intended landing site? Also no one has real good windmill vs stopped prop numbers. There has to be a trade off. Again unless I am real high and no chance of getting the engine started such as catastro phic failure vs carb ice that might melt and allow engine to start at lower (warmer) altitudes, than I am dubious at how practical it is. No argument stopped is less drag. Cheers George Glide ratio , glide distance , power off landing ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: Tip up Canopy Vs. Slider
Date: May 02, 2005
I would not venture into making a statement like Yes to your question. But I will venture out onto the limb of no return and suggest that tip ups are easier to get airtight than sliders. I have a tip up and the canopy is very tight at the back and most slider folks have to work at for some time to make that claim. The tip up sides are very tight IF the canopy frame is built and installed correctly. Indiana Larry, RV7 Tip Up FLYING - Phase 1 ----- Original Message ----- From: "RV3 PILOT" <RMCKEE(at)MN.RR.COM> Subject: RV-List: Tip up Canopy Vs. Slider > > I would like to know if the tip up canopies seal better than the sliders > do around the fuselage sides? I have heard that the sliders leak a fair > amount of air around the sides of the canopy in flight. If anyone can > help me out with this please e-mail me. > > Robin > RV3B Kit 11356 > Minnesota > RMCKEE(at)MN.RR.COM > > > ________________________________________________________________________________
Date: May 02, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: try-it-yourself fly-in - was Long glide to landing
On 22:25:34 2005-05-01 "Greg Young" <gyoung@cs-sol.com> wrote: > I beg to differ - windmilling IS the realistic condition. If the power > stops either because of lack of fuel or ignition and the prop keeps > windmilling at glide speed then that's what you should > simulate/practice. At low altitude you have to take what you get. There are more factors to consider than just whether the prop is windmilling. Is the engine running at all, ie. idling? Then it's producing *some* power. If the engine isn't running, and the drag in the system is just the pistons moving around, then the prop is creating drag that can be removed by stopping the prop. If the crankshaft has failed and the prop is windmilling in its front bearing, then the prop is *really* windmilling, and that creates a *lot* of drag (but I don't know off the top of my head if it's more or less than with an idling engine... It may depend on the airframe). Anyone who doubts that a windmilling prop creates more drag than a stopped one, go buy one of those styrofoam punch-out airplanes that has just a windmilling prop on it. Fly it once with the prop windmilling, and fly it agan with the prop taped in place. You'll consistently get more distance out of it with the prop stopped. The result is even more dramatic if you try this with one of those balsa stick-models. Fly it once with the rubber band removed, and fly it again with the prop taped in place. -Rob ________________________________________________________________________________
Date: May 02, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
On 6:42:30 2005-05-02 linn walters wrote: > I think it would be a great exercise to see just > how easy/hard it is to stop the prop ..... and keep it stopped ..... > and then see what the real-world differences there are. Linn That's an excellent point, Linn, and I forgot to mention that. It's worth noting that a wood prop has a lot less momentum, and is a lot easier to stop, than a metal one. When we tried this while I was learning to fly, it was in a Cessna 152 with a metal prop. We did have to pull the nose up about 30 degrees and hold it there for a moment to get the blades to stop turning. Once it was stopped, we could establish best glide (and even a bit faster) without it starting again, although it did rotate about 1/8 turn until it hit the compression stroke. My recollection was that we had to get it up to about 90mph before it would turn over on it's own. In contrast, I tried the same thing on a wood-propped homebuilt, and the prop stopped dead the second I pulled the mixture, without me even lifting the nose. The silence was even more deafening because I wasn't expecting it... I thought I would have to raise the nose at least a bit to get it to stop. In this case, I couldn't get the prop to start turning again without using the starter, although I dove to 110mph first to try it. In a wood propped homebuilt, I would have no second thoughts about stopping the prop. In a metal propped one, I would probably only bother trying if I were (a) behind a constant speed prop or (b) at a sufficiently high altitude when it quit. -Rob ________________________________________________________________________________
From: "BRUCE GRAY" <brucerv84us(at)hotmail.com>
Subject: CARSON CITY, NV. FLY-IN
Date: May 02, 2005
Hello Everyone, Just wanted to send out a quick e-mail to everyone in the RV community that the Carson City, NV. Chapter 403 is hosting its 2nd Annual RV Fly-in. We have factory support and weather permitting will have Ken Scott there with a Demo aircraft for potential builders to get a taste. You can find more info. on the Chapter web sight at www.eaa403.org. The airport identifier is CXP. We hope you can make it out to this fly-in and make this a growing event. Last year we counted 31 RV aircraft which included the "EXXON FLYING TIGER" and the 1st Factory built RV10. If you are not able to make it please spread the word for the ones that could and didn't get the word. Thank You, Bruce Gray RV8 Fuselage coming soon ________________________________________________________________________________
From: "Mark Banus" <mbanus(at)hotmail.com>
Subject: Airport Identifiers
Date: May 02, 2005
Try AirNav http://www.airnav.com/ Mark Banus ________________________________________________________________________________
From: "Moore, Warren" <Warren.Moore(at)tidelandsoil.com>
Subject: Joe Banos - Transition Training
Date: May 02, 2005
I understand Joe Banos is giving transition training in the San Diego area in his RV-6....does anyone have his contact information? eJ8+IggUAQaQCAAEAAAAAAABAAEAAQeQBgAIAAAA5AQAAAAAAADoAAEIgAcAGAAAAElQTS5NaWNy b3NvZnQgTWFpbC5Ob3RlADEIAQWAAwAOAAAA1QcFAAIADQA5AAQAAQAuAQEggAMADgAAANUHBQAC AA0AOQAHAAEAMQEBCYABACEAAABCNUEwRTAyMTZGOEJBRjQ4OTMwQjNCQjkzQjg2NDlDQwBNBwEE gAEAIAAAAEpvZSBCYW5vcyAtIFRyYW5zaXRpb24gVHJhaW5pbmcAJQsBDYAEAAIAAAACAAIAAQOQ BgCABgAAMAAAAAMAW4AIIAYAAAAAAMAAAAAAAABGAAAAAFKFAAAnagEAHgBcgAggBgAAAAAAwAAA AAAAAEYAAAAAVIUAAAEAAAAEAAAAOS4wAAsAgIAIIAYAAAAAAMAAAAAAAABGAAAAAAaFAAAAAAAA AwAOgAggBgAAAAAAwAAAAAAAAEYAAAAAAYUAAAAAAAALABCACCAGAAAAAADAAAAAAAAARgAAAAAD hQAAAAAAAAsAEYAIIAYAAAAAAMAAAAAAAABGAAAAAA6FAAAAAAAAAwA3gAggBgAAAAAAwAAAAAAA AEYAAAAAEIUAAAAAAAADADiACCAGAAAAAADAAAAAAAAARgAAAAARhQAAAAAAAAMAPoAIIAYAAAAA AMAAAAAAAABGAAAAABiFAAAAAAAAHgBLgAggBgAAAAAAwAAAAAAAAEYAAAAANoUAAAEAAAABAAAA AAAAAB4ATIAIIAYAAAAAAMAAAAAAAABGAAAAADeFAAABAAAAAQAAAAAAAAAeAE2ACCAGAAAAAADA AAAAAAAARgAAAAA4hQAAAQAAAAEAAAAAAAAAAgEJEAEAAADdAAAA2QAAAPsAAABMWkZ1vMFWTQMA CgByY3BnMTI1FjIA+Atgbg4QMDMzTwH3AqQD4wIAY2gKwHOwZXQwIAcTAoB9CoGSdgiQd2sLgGQ0 DGAOYwBQCwMLtSBJIHUbEoAEkHMBkBKAIEpvaGUgQgBwbwQgBAAgjGdpEiAPICB0cgBy/HRpAiAV 0guAFaILgBXQJmgUwAYRIEQIkGdvUiAKwGVhFxJoFUFS0FYtNi4ZMWQUsAQg3QBweQIgFMAQ8HYa ERVBvwWgAjAA0AVAC4ACEHIAwF0WQj8KogqAEeEAHKAAAAAeAHAAAQAAACAAAABKb2UgQmFub3Mg LSBUcmFuc2l0aW9uIFRyYWluaW5nAAIBcQABAAAAFgAAAAHFT1mefo1OV0y7ERHZjBQAAuMJYvYA AAMAJgAAAAAAAwA2AAAAAAALAAIAAQAAAAMACVkDAAAAAwDeP69vAABAADkAYA6FfllPxQEDAPE/ CQQAAB4AMUABAAAADQAAAFdBUlJFTiBNT09SRQAAAAADABpAAAAAAB4AMEABAAAADQAAAFdBUlJF TiBNT09SRQAAAAADABlAAAAAAAMA/T/kBAAAAwCAEP////8CAUcAAQAAADYAAABjPVVTO2E9IDtw PVRpZGVsYW5kcyBPaWw7bD1MT0NVVFVTLTA1MDUwMjIwNTcwNFotMTY0MwAAAAIB+T8BAAAAVAAA AAAAAADcp0DIwEIQGrS5CAArL+GCAQAAAAAAAAAvTz1USURFTEFORFMgT0lML09VPU5FWFVTL0NO PVJFQ0lQSUVOVFMvQ049V0FSUkVOIE1PT1JFAB4A+D8BAAAADgAAAE1vb3JlLCBXYXJyZW4AAAAe ADhAAQAAAA0AAABXQVJSRU4gTU9PUkUAAAAAAgH7PwEAAABUAAAAAAAAANynQMjAQhAatLkIACsv 4YIBAAAAAAAAAC9PPVRJREVMQU5EUyBPSUwvT1U9TkVYVVMvQ049UkVDSVBJRU5UUy9DTj1XQVJS RU4gTU9PUkUAHgD6PwEAAAAOAAAATW9vcmUsIFdhcnJlbgAAAB4AOUABAAAADQAAAFdBUlJFTiBN T09SRQAAAABAAAcwIEZ76lhPxQFAAAgwQNFEgFlPxQEeAD0AAQAAAAEAAAAAAAAAHgAdDgEAAAAg AAAASm9lIEJhbm9zIC0gVHJhbnNpdGlvbiBUcmFpbmluZwAeADUQAQAAAEIAAAA8QTFGMkI5MEM2 MkY0RDMxMUJCMTgwMDUwOEI4QkZDMUMxNzNBODdAbG9jdXR1cy50aWRlbGFuZHNvaWwuY29tPgAA AAsAKQAAAAAACwAjAAAAAAADAAYQt0HZgwMABxBrAAAAAwAQEAAAAAADABEQAAAAAB4ACBABAAAA ZQAAAElVTkRFUlNUQU5ESk9FQkFOT1NJU0dJVklOR1RSQU5TSVRJT05UUkFJTklOR0lOVEhFU0FO RElFR09BUkVBSU5ISVNSVi02RE9FU0FOWU9ORUhBVkVISVNDT05UQUNUSU5GT1IAAAAAAgF/AAEA AABCAAAAPEExRjJCOTBDNjJGNEQzMTFCQjE4MDA1MDhCOEJGQzFDMTczQTg3QGxvY3V0dXMudGlk ZWxhbmRzb2lsLmNvbT4AAAAhPQ= ________________________________________________________________________________
Date: May 02, 2005
From: Chris W <1qazxsw23edcvfr45tgbnhy67ujm(at)cox.net>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Garth Shearing wrote: > >And I beg to differ with you, Greg. If you want minimum sink rate, low >drag, and maximum distance to glide, you have to reduce speed to stop the >prop, and then increase speed to best glide ratio. In the unlikely event >that the best glide ratio speed restarts the windmilling, then use a >slightly lower glide speed. In an engine out emergency, that is the >realistic and best condition. > >Don't ask me how I know. > > > How slow did you have to go to get the prop to stop? While I agree that it would be best to stop the prop and then go to best glide speed, if you are say less than 3000 ft AGL, don't you think there would be too little time to do that? Once I get my ticket and build my -7, I don't ever plan on being much less than 8,000 ft AGL except for takeoff & landing, very short trips and when crossing mountain peaks. In my part of the country 8,000 ft AGL isn't hard to do and with that much room, if the engine quits, you generally have at least 2 airports with in gliding range. -- Chris W ________________________________________________________________________________
Date: May 02, 2005
From: Bob J <rocketbob(at)gmail.com>
Subject: Re: Lower cowl movement estimate
If you do aerobatics, you'll need 1" clearance minimum. I had to change the alternator arm and go to a shorter belt, obviously that involved taking the prop off. What a pain in the butt that was. This was after my alternator pulley started wearing into the cowl, and of course long after reading in the archives that 1/2" clearance was plenty. Doing point rolls are what started my cowl rubbing...I suspect the mounts aren't as stiff along that axis of engine movement. Regards, Bob Japundza RV-6 flying 600+ hours F1 under const. On 5/1/05, DAVID REEL wrote: > > Does anybody have an estimate for how far up the lower cowl on an RV8A would move in flight? I have the epoxy honeycomb sandwich type cowl shipped about 5 years ago. I'm wondering how much alternator pulley clearance I need to provide & why we don't align our filtered air box and cowl air inlets with the cowl displaced upwards. > > Upon researching the archives, engine sag when pulling G's rather than cowl movement due to aerodynamic pressure may be the problem. But the need is still the same. Virtually nobody gives actual clearances static or otherwise, nor do they mention the direction of movement. I know that many have experienced alternator pulley contact problems & feel whatever hard numbers or even estimated numbers anyone could provide would be very helpful. Imagine if someone noted that they had 1/4" vertical clearance & experienced chafing, increased it to 3/4" & had no further problem. Even a few people reporting how much clearance they had & that there was no problem would be great. Next time your top cowl is off, how about sticking a drill or a small piece of wood in between whatever is closest and your cowl & let us all know your actual clearance & whether there has been contact? > > Dave Reel - RV8A > > > ________________________________________________________________________________
Date: May 02, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: IO-320 in 9(A)/Catto props
First of all, for anybody who followed the thread, I did decide to go with the 9A over the 7. I was originally going to just put my order on hold until I got a chance to fly both the 7A and 9A but did enough research and got enough private mails from people on the list to convince me. And I'm never going to get the chance to fly either in IMC as a demo anyway. I sort of liked the possibility of sport aerobatics at some point but XC and especially IFR suitability and stability are much more important to me. Can't have everything. (It wasn't that I didn't know the differences between the 9 and the 7 - I did - but I guess I had convinced myself that since many ppl fly IFR in 6s/7s, I could too. And maybe I could, but I'd rather have the stable ride. Single-pilot IMC in my C-152 is demanding enough for me - I'd rather not increase the workload.) Going to the 9 is fitting, though, since seeing the 9A prototype at OSH 2000 was what initially inspired me to get my PPL. It was the first kitplane I ever wanted, and now I've come full-circle indeed. (I was almost embarrassed to call Van's again after just changing my order from a 10 to a 7A, but the girl laughed and said this is not terribly uncommon. They hadn't started putting together my QB kit.) Question regarding engines. I'm not at all sure I'd want to go FI (I'm trying to keep the costs down, since my panel is gonna cost a bundle, and I like the simplicity of the carb), but I noticed that Van's offers no FWF kit for the IO-320. I am sure there are those out there with FI 320s - how much of a pain was it? Where is your servo mounted? Are you using the stock cowl with the scoop? 2nd question: Experiences with the 3-bladed Catto prop? It looks to me like they make great stuff. I did search the archive and see some positive reports. I would be really interested in seeing numbers to compare to the 79 pitch Sensenich that Van's recommends. TIA. ________________________________________________________________________________
Date: May 02, 2005
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Long glide to landing
> >3. Whats a typical glide ratio for a constant speed prop? I doubt there's >much difference between models. > There actually might be a fair difference in windmilling drag between different constant-speed prop setups. The following items may be significant: 1. If there is no oil pressure: Which way the prop pitch goes when it losses oil pressure. Some props are designed to go to high pitch with low oil pressure, some go to low pitch. In particular, the Hartzells that most people use go to low pitch. 2. If there is oil pressure: What is the rpm selected by the prop control, and how does that compare to the windmilling rpm? If the prop is windmilling at a lower rpm than that which is selected by the prop control, then the prop will be at the pitch defined by its low pitch stop (i.e. lots of drag). 3. If there is oil pressure: Has the pilot pulled the prop control full aft, and if so, is the minimum selectable rpm less than the windmilling rpm? If so, the prop will go to high pitch (i.e. less drag). 4. If the prop is sitting on the low pitch stop, has the owner adjusted the low pitch stop to be at as high a pitch as possible? If you want minimum drag when the prop is windmilling, the low pitch stop should be adjusted as high as possible. Ideally, the low pitch stop should be adjusted high enough so the prop doesn't come up to full rpm until the aircraft has some airspeed. The rpm during the first part of the take-off roll should be less than the governing rpm, as the prop would be limited by the low pitch stop. The rpm would increase as the speed increased, and reach governing rpm late in the take-off roll. -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net>
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 02, 2005
> > Just one more thought to unfuel the fire (pun intended) > > If you want to extend your glide with a windmilling prop then > keep the > throttle wide open (assuming it is not running) to reduce > the pumping > losses. Vic, I believe least drag would be with the throttle closed. Consider the intake stroke - yes, there would be power needed to pull the piston down against the lower manifold pressure. However, most of that would be recovered during the "compression" stroke, when this same lower pressure in the cylinder "pulls" the piston back up. With the throttle open, a full charge of air approximately at ambient pressure needs to be compressed to around 125 psi on the compression stroke, being released suddenly into the exhaust pipe when the exhaust valve opens. Alex Peterson RV6-A 612 hours Maple Grove, MN http://www.home.earthlink.net/~alexpeterson/ ________________________________________________________________________________
Date: May 02, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: IO-320 in 9(A)/Catto props
I think the Catto Prop is a great product. I emailed them for detailed information but never got a reponse? Folbrecht First of all, for anybody who followed the thread, I did decide to go with the 9A over the 7. I was originally going to just put my order on hold until I got a chance to fly both the 7A and 9A but did enough research and got enough private mails from people on the list to convince me. And I'm never going to get the chance to fly either in IMC as a demo anyway. I sort of liked the possibility of sport aerobatics at some point but XC and especially IFR suitability and stability are much more important to me. Can't have everything. (It wasn't that I didn't know the differences between the 9 and the 7 - I did - but I guess I had convinced myself that since many ppl fly IFR in 6s/7s, I could too. And maybe I could, but I'd rather have the stable ride. Single-pilot IMC in my C-152 is demanding enough for me - I'd rather not increase the workload.) Going to the 9 is fitting, though, since seeing the 9A prototype at OSH 2000 was what initially inspired me to get my PPL. It was the first kitplane I ever wanted, and now I've come full-circle indeed. (I was almost embarrassed to call Van's again after just changing my order from a 10 to a 7A, but the girl laughed and said this is not terribly uncommon. They hadn't started putting together my QB kit.) Question regarding engines. I'm not at all sure I'd want to go FI (I'm trying to keep the costs down, since my panel is gonna cost a bundle, and I like the simplicity of the carb), but I noticed that Van's offers no FWF kit for the IO-320. I am sure there are those out there with FI 320s - how much of a pain was it? Where is your servo mounted? Are you using the stock cowl with the scoop? 2nd question: Experiences with the 3-bladed Catto prop? It looks to me like they make great stuff. I did search the archive and see some positive reports. I would be really interested in seeing numbers to compare to the 79 pitch Sensenich that Van's recommends. TIA. Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) ________________________________________________________________________________
From: "RV6 Flyer" <rv6_flyer(at)hotmail.com>
Subject: Joe Banos - Transition Training
Date: May 03, 2005
From the SoCAL Group "Joe Banos" "Not sure who to direct this to. I am a Certified Flight Instructor (30 years), former military pilot and RV-6 owner in the San Diego area. I have the FAA excemption for transition training and would like to make myself available for RV training of builders or buyers in the So Cal area. Is it proper to disseminate this info or notify the group via this means?" JoeB Gary A. Sobek "My Sanity" RV-6 N157GS O-320 Hartzell, 1,665 + Flying Hours So. CA, USA http://SoCAL_WVAF.rvproject.com --- -Original Message Follows---- From: "Moore, Warren" <Warren.Moore(at)TidelandsOil.com> Subject: RV-List: Joe Banos - Transition Training Date: Mon, 2 May 2005 13:57:04 -0700 I understand Joe Banos is giving transition training in the San Diego area in his RV-6....does anyone have his contact information? ________________________________________________________________________________
Date: May 02, 2005
From: Dave Bristol <dbris200(at)sbcglobal.net>
Subject: Re: Long glide to landing
If there is NO oil pressure, you really don't have to worry about it, since it's probably going to stop turning pretty soon anyway. 8 >) Dave Kevin Horton wrote: > > >There actually might be a fair difference in windmilling drag between >different constant-speed prop setups. The following items may be >significant: > >1. If there is no oil pressure: Which way the prop pitch goes when it >losses oil pressure. Some props are designed to go to high pitch >with low oil pressure, some go to low pitch. In particular, the >Hartzells that most people use go to low pitch. > > > > ________________________________________________________________________________
From: "Jeff Orear" <jorear(at)new.rr.com>
Subject: Re: IO-320 in 9(A)/Catto props
Date: May 02, 2005
----- Original Message ----- From: "Darrell Reiley" <lifeofreiley2003(at)yahoo.com> Subject: Re: RV-List: IO-320 in 9(A)/Catto props > > I think the Catto Prop is a great product. I emailed them for detailed > information but never got a reponse? Darrell: Craig Catto is a very busy guy lately, with all us RV guys sending business his way. Hopefully he has not responded to your email because he is busy working on my prop!! ; ) Best way to contact him is to give him a call. Regards, Jeff Orear RV6A N782P (reserved) moving to the airport on 5/11 Peshtigo, WI ________________________________________________________________________________
Date: May 02, 2005
Subject: [ Mike Holland ] : New Email List Photo Share Available!
From: Email List Photo Shares <pictures(at)matronics.com>
A new Email List Photo Share is available: Poster: Mike Holland Lists: RV-List,RV6-List,RV7-List,RV8-List,RV9-List,RV10-List Subject: Quickbuild Fuel Pickup Issue http://www.matronics.com/photoshare/hollandm@pacbell.net.05.02.2005/index.html o Main Photo Share Index http://www.matronics.com/photoshare o Submitting a Photo Share If you wish to submit a Photo Share of your own, please include the following information along with your email message and files: 1) Email List or Lists that they are related to: 2) Your Full Name: 3) Your Email Address: 4) One line Subject description: 5) Multi-line, multi-paragraph description of topic: 6) One-line Description of each photo or file: Email the information above and your files and photos to: pictures(at)matronics.com ________________________________________________________________________________
Date: May 02, 2005
Subject: [ Rob Ray ] : New Email List Photo Share Available!
From: Email List Photo Shares <pictures(at)matronics.com>
A new Email List Photo Share is available: Poster: Rob Ray Lists: RV-List,RV4-List Subject: RV4 canopy hold-open latch http://www.matronics.com/photoshare/smokyray@yahoo.com.05.02.2005/index.html o Main Photo Share Index http://www.matronics.com/photoshare o Submitting a Photo Share If you wish to submit a Photo Share of your own, please include the following information along with your email message and files: 1) Email List or Lists that they are related to: 2) Your Full Name: 3) Your Email Address: 4) One line Subject description: 5) Multi-line, multi-paragraph description of topic: 6) One-line Description of each photo or file: Email the information above and your files and photos to: pictures(at)matronics.com ________________________________________________________________________________
Date: May 02, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: IO-320 in 9(A)/Catto props
Same here. Probably just doesn't check email often. Seems to be a very small operation. I'll give him a call in a week or two if he doesn't write back. One concern I would have would be regarding vibration testing. Has it been done with his props? With what engines? Have you ever read the RVator article about the necessity for real vibration testing for every prop/engine combination? It is indeed a necessity. Another (minor) area would be concerning the flyoff period - no 25 hour period with that prop. Then again I don't think the experimental Lycs could ever qualify for that anyway? --- Darrell Reiley wrote: > > I think the Catto Prop is a great product. I emailed them for detailed > information but never got a reponse? > > Paul Folbrecht > > > First of all, for anybody who followed the thread, I did decide to go with > the > 9A over the 7. I was originally going to just put my order on hold until I > got > a chance to fly both the 7A and 9A but did enough research and got enough > private mails from people on the list to convince me. And I'm never going to > get the chance to fly either in IMC as a demo anyway. I sort of liked the > possibility of sport aerobatics at some point but XC and especially IFR > suitability and stability are much more important to me. Can't have > everything. > > (It wasn't that I didn't know the differences between the 9 and the 7 - I did > - > but I guess I had convinced myself that since many ppl fly IFR in 6s/7s, I > could too. And maybe I could, but I'd rather have the stable ride. > Single-pilot IMC in my C-152 is demanding enough for me - I'd rather not > increase the workload.) > > Going to the 9 is fitting, though, since seeing the 9A prototype at OSH 2000 > was what initially inspired me to get my PPL. It was the first kitplane I > ever > wanted, and now I've come full-circle indeed. (I was almost embarrassed to > call Van's again after just changing my order from a 10 to a 7A, but the girl > laughed and said this is not terribly uncommon. They hadn't started putting > together my QB kit.) > > Question regarding engines. I'm not at all sure I'd want to go FI (I'm trying > to keep the costs down, since my panel is gonna cost a bundle, and I like the > simplicity of the carb), but I noticed that Van's offers no FWF kit for the > IO-320. I am sure there are those out there with FI 320s - how much of a pain > was it? Where is your servo mounted? Are you using the stock cowl with the > scoop? > > 2nd question: Experiences with the 3-bladed Catto prop? It looks to me like > they make great stuff. I did search the archive and see some positive > reports. > I would be really interested in seeing numbers to compare to the 79 pitch > Sensenich that Van's recommends. > > TIA. > > > Darrell Reiley > Round Rock, Texas > RV 7A #70125 > N622DR (reserved) > > > > > > > > ________________________________________________________________________________
From: "randall" <rv6n6r(at)comcast.net>
Subject: Re: Tip up Canopy Vs. Slider
Date: May 02, 2005
The slider is indeed difficult to seal on the sides. Mine fits as tight as any I've seen, but even if done perfectly there're still gaps that are hard to completely seal with any kind of seal material, due to the geometry when it opens and closes. In fact I wouldn't mind hearing from others as to how they did that. No water comes in and I fly in the rain a fair amount, and I don't notice the cold air except on really cold days. But there's a fair amount of wind noise from the gaps at the back that I just can't seam to seal, and I'd like to get it as quiet as I can. Randall Henderson, RV-6 Portland, OR >> > > I would like to know if the tip up canopies seal better than the sliders > > do around the fuselage sides? I have heard that the sliders leak a fair > > amount of air around the sides of the canopy in flight. If anyone can > > help me out with this please e-mail me. > > > > Robin > > RV3B Kit 11356 > > Minnesota > > RMCKEE(at)MN.RR.COM > > > > > > > > ________________________________________________________________________________
Date: May 02, 2005
From: Alison and Neil <alisonandneil(at)direcway.com>
Subject: Re: Joe Banos - Transition Training
Joe, Yes, absolutely. In fact I've been looking for someone closer than TX or WA. I'll be in touch. Neil McLeod 7 QB Finishing ----- Original Message ----- From: "RV6 Flyer" <rv6_flyer(at)hotmail.com> Subject: RE: RV-List: Joe Banos - Transition Training > > From the SoCAL Group > > "Joe Banos" > > "Not sure who to direct this to. I am a Certified Flight Instructor > (30 years), former military pilot and RV-6 owner in the San Diego > area. I have the FAA excemption for transition training and would > like to make myself available for RV training of builders or buyers in > the So Cal area. Is it proper to disseminate this info or notify the > group via this means?" > > JoeB > > > Gary A. Sobek > "My Sanity" RV-6 N157GS O-320 Hartzell, > 1,665 + Flying Hours So. CA, USA > http://SoCAL_WVAF.rvproject.com > > --- > -Original Message Follows---- > From: "Moore, Warren" <Warren.Moore(at)TidelandsOil.com> > To: "'RV List'" > Subject: RV-List: Joe Banos - Transition Training > Date: Mon, 2 May 2005 13:57:04 -0700 > > > > I understand Joe Banos is giving transition training in the San Diego area > in his RV-6....does anyone have his contact information? > > ________________________________________________________________________________
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 03, 2005
From: "Greg Young" <gyoung@cs-sol.com>
It seems we're really arguing the definition of "realistic." I will agree that a stopped prop represents the lowest drag configuration which in turn nets better sink and glide ratio. What I don't agree with is whether it is "realistic" (or wise) to do what it takes to get the prop stopped in any given engine out. If it occurs at 400 AGL and 80 mph I would assert that it is decidedly unwise as you'll be on the ground in 10-15 seconds. At 10,000 AGL and 170 kts you have more freedom to optimize things. Somewhere in between there's a transition point from unwise to possible to desireable. Slowing the aircraft below best glide speed to stop the prop and then regaining airspeed to best glide involves some loss of gliding range. How much and whether you can recover it with the lower drag (and how long it takes) is anyones guess. There are 4000 RVs flying and over a thousand folks on this list and I've still not seen any performance data solid enough to do that kind of trade-off study with any confidence. So we're left with our judgement to decide. My reasoning is that at low altitude (pick your own definition, 0-3K AGL?) your options are most limited and fast and correct decisions are most critical. It's not the time to approach stall in an emergency and you've got enough other things to do in the time remaining. At high altitude you may have many more options so the ability to eek out the last bit of glide range may not be that valuable. You're likely to gain more by correctly judging the effect of the wind on your range and available airports. At any event I would leave stopping the prop until after all the essentials are completed and all restart attempts are done. At that point you've lost more altitude and marginalized the benefits somewhat. My view of "realistic" is what is conservatively attainable in real world conditions. For the reasons above I don't think stopping the prop is reasonable or even possible in many cases and therefore objected to calling it THE realistic condition. It's certainly subjective so YMMV. Regardless of your view, it's important to periodically evaluate your views and practices. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A > > And I beg to differ with you, Greg. If you want minimum sink > rate, low drag, and maximum distance to glide, you have to > reduce speed to stop the prop, and then increase speed to > best glide ratio. In the unlikely event that the best glide > ratio speed restarts the windmilling, then use a slightly > lower glide speed. In an engine out emergency, that is the > realistic and best condition. > > Don't ask me how I know. > > Garth Shearing > VariEze & 90% RV6A > Victoria BC Canada > ________________________________________________________________________________
Date: May 03, 2005
From: Jeff Point <jpoint(at)mindspring.com>
Subject: Re: IO-320 in 9(A)/Catto props
I'll second what others have written about communicating with Craig. I just bought a prop from him (took delivery three days before leaving for SnF) and had a lot of communication back and forth. He had computer problems so email was out. He always answers the phone or returns calls quickly. Very good guy to deal with. He did tell me that about 90% of his business nowadays is making 3 blade props for RVs. My prop is a 3 blade Catto, 66 inch pitch and 76 inch pitch. It is on an Aerosport Power/ Superior O-360, carb, 8.5 pistons, one mag and one Lightspeed II ignition. Pretty stock engine. I talked with Craig at some length about the prop pitch. I explained that I wanted a prop which was not quite a cruise, but closer to a cruise than a climb prop. The Sterba wood prop which it replaced (and is now on Ebay if anyone is interested- shameless plug) was just such a prop. I was willing to sacrifice a couple knots of top end for better short field performance. Craig assured me that I would see an increase in top end with no loss of acceleration or short field performance. Well, the proof is in the pudding. I saw about a 5 kt increase in cruise (75%, 8K ft standard) from 172 to 177 ktas. I hit 180 ktas at 4500 ft racing a 200HP/ Hartzell blended airfoil RV-8 (I was nose to nose with him at full throttle for several minutes, until he pushed the RPM up past 2400!) I saw a pretty substantial decrease in static RPM (around 180 or so) but seem to have no loss of acceleration or takeoff distance. I guess the prop produces more thrust at lower RPM than the old one. As for real world cruise- around 2500 RPM gives TAS in the low 160s with burns around 8.5-9 GPH, depending on altitude. A fixed pitch prop just has to turn too damn fast to get real power out of the engine, but gas is expensive and I like to baby the engine anyway. The prop changed the feel of the engine a lot. It now feels and sounds more like a 6 cylinder engine than a 4 banger. I can't say it's quieter, but it's a different, higher frequency type of noise. There are a couple rough RPM ranges down low. Not any more so than with my old prop, but it seems more noticable in comparison. I have yet to get it dynamically balanced but that is in the works. One more thing- my wheel landings seem to have gotten better. I think that subconsciously I am no longer worried about a prop strike with the small diameter prop;) Oh, one more thing- it looks cool as hell! Jeff Point RV-6 Milwaukee WI > > ________________________________________________________________________________
Date: May 03, 2005
From: Doug Gray <dgra1233(at)bigpond.net.au>
Subject: Re: Tip up Canopy Vs. Slider
> If you block up the slider during fitting and assembly of the aft skirts, > they will then fit quite nice and snug when you remove the blocks. The only > air/rain we have that leaks into the slider is the very tiny bit that comes in > around the sliding rail cap at the top due to the low pressure in this area. > One of these days I'll fashion a way to plug this area. > > IMO the slider is a pretty tight fit if done well. > > > GV (RV-6A N1GV O-360-A1A, C/S, Flying 742hrs, Silicon Valley, CA) > How high did you block the slider for this method? Also, how did you seal the side skirts? Doug Gray On approach to slider anxiety... ________________________________________________________________________________
Date: May 03, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: IO-320 in 9(A)/Catto props
Will do... I just know how phone calls all day can pull people off task. Emails can be answered at their convenience... You would think it would help? Darrell Jeff Orear wrote: ----- Original Message ----- From: "Darrell Reiley" Subject: Re: RV-List: IO-320 in 9(A)/Catto props > > I think the Catto Prop is a great product. I emailed them for detailed > information but never got a reponse? Darrell: Craig Catto is a very busy guy lately, with all us RV guys sending business his way. Hopefully he has not responded to your email because he is busy working on my prop!! ; ) Best way to contact him is to give him a call. Regards, Jeff Orear RV6A N782P (reserved) moving to the airport on 5/11 Peshtigo, WI Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: IO-320 in 9(A)/Catto props
Date: May 03, 2005
Vibration is generally not an issue with non-metallic props as they are self dampening. Cy Galley - Chair, AirVenture Emergency Aircraft Repair A Service Project of Chapter 75 EAA Safety Programs Editor - TC EAA Sport Pilot ----- Original Message ----- From: "Paul Folbrecht" <paulfolbrecht(at)yahoo.com> Subject: Re: RV-List: IO-320 in 9(A)/Catto props > > Same here. Probably just doesn't check email often. Seems to be a very > small > operation. I'll give him a call in a week or two if he doesn't write > back. > > One concern I would have would be regarding vibration testing. Has it > been > done with his props? With what engines? Have you ever read the RVator > article > about the necessity for real vibration testing for every prop/engine > combination? It is indeed a necessity. > > Another (minor) area would be concerning the flyoff period - no 25 hour > period > with that prop. Then again I don't think the experimental Lycs could ever > qualify for that anyway? > > --- Darrell Reiley wrote: >> >> >> I think the Catto Prop is a great product. I emailed them for detailed >> information but never got a reponse? >> >> Paul Folbrecht wrote:--> RV-List message posted >> by: >> Paul Folbrecht >> >> >> First of all, for anybody who followed the thread, I did decide to go >> with >> the >> 9A over the 7. I was originally going to just put my order on hold until >> I >> got >> a chance to fly both the 7A and 9A but did enough research and got enough >> private mails from people on the list to convince me. And I'm never going >> to >> get the chance to fly either in IMC as a demo anyway. I sort of liked the >> possibility of sport aerobatics at some point but XC and especially IFR >> suitability and stability are much more important to me. Can't have >> everything. >> >> (It wasn't that I didn't know the differences between the 9 and the 7 - I >> did >> - >> but I guess I had convinced myself that since many ppl fly IFR in 6s/7s, >> I >> could too. And maybe I could, but I'd rather have the stable ride. >> Single-pilot IMC in my C-152 is demanding enough for me - I'd rather not >> increase the workload.) >> >> Going to the 9 is fitting, though, since seeing the 9A prototype at OSH >> 2000 >> was what initially inspired me to get my PPL. It was the first kitplane I >> ever >> wanted, and now I've come full-circle indeed. (I was almost embarrassed >> to >> call Van's again after just changing my order from a 10 to a 7A, but the >> girl >> laughed and said this is not terribly uncommon. They hadn't started >> putting >> together my QB kit.) >> >> Question regarding engines. I'm not at all sure I'd want to go FI (I'm >> trying >> to keep the costs down, since my panel is gonna cost a bundle, and I like >> the >> simplicity of the carb), but I noticed that Van's offers no FWF kit for >> the >> IO-320. I am sure there are those out there with FI 320s - how much of a >> pain >> was it? Where is your servo mounted? Are you using the stock cowl with >> the >> scoop? >> >> 2nd question: Experiences with the 3-bladed Catto prop? It looks to me >> like >> they make great stuff. I did search the archive and see some positive >> reports. >> I would be really interested in seeing numbers to compare to the 79 pitch >> Sensenich that Van's recommends. >> >> TIA. >> >> >> Darrell Reiley >> Round Rock, Texas >> RV 7A #70125 >> N622DR (reserved) >> >> >> >> >> >> >> >> > > > ________________________________________________________________________________
From: "Vic Jacko" <vicwj(at)earthlink.net>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 03, 2005
Alex, I believe you may be correct. I would be good if someone had a chance to test the drag in both configurations. Thanks for you insight. Vic ----- Original Message ----- From: "Alex & Gerry Peterson" <alexpeterson(at)earthlink.net> Subject: RE: RV-List: try-it-yourself fly-in - was Long glide to landing > > > >> >> Just one more thought to unfuel the fire (pun intended) >> >> If you want to extend your glide with a windmilling prop then >> keep the >> throttle wide open (assuming it is not running) to reduce >> the pumping >> losses. > > Vic, I believe least drag would be with the throttle closed. Consider the > intake stroke - yes, there would be power needed to pull the piston down > against the lower manifold pressure. However, most of that would be > recovered during the "compression" stroke, when this same lower pressure > in > the cylinder "pulls" the piston back up. With the throttle open, a full > charge of air approximately at ambient pressure needs to be compressed to > around 125 psi on the compression stroke, being released suddenly into the > exhaust pipe when the exhaust valve opens. > > Alex Peterson > RV6-A 612 hours > Maple Grove, MN > > http://www.home.earthlink.net/~alexpeterson/ > > > ________________________________________________________________________________
From: "Vincent Welch" <welchvincent(at)hotmail.com>
Subject: Fuel Senders
Date: May 03, 2005
Gentlemen, I am having a problem with my SW fuel senders. It seems that the floats are sticking at the pivot point. I removed the units and I can move the floats by hand but when I lift the float to the full position and release it, it remains. If I shake or jiggle it, the float will drop. Is there some way to free up the mechanism? I am afraid that as I burn fuel, the sender won't follow the level. Any ideas? Vince RV-8A ________________________________________________________________________________
Subject: Awesome Missouri flyin this weekend
Date: May 03, 2005
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
"Flash"! THIRD ANNUAL REBEL'S BLUFF FLYIN Now that Sun n Fun is over, it's time to fly to the Third Annual Rebel's Bluff FlyIn for Rocket's and Van's RV Aircraft on May 7th, 2005. Come in about 10:00AM for an Ozarks Style Bar-B-Que lunch with all the fixin's (catered by the First Baptist Ladies Group), and some great comaradrie. Rebel's Bluff (N37 06.1 W93 52.2) is located two miles north of Mt Vernon Municipal Airport (2MO), and just west of Mt Vernon, Missouri. About 150 miles SSE of Kansas City, MO, and 140 east of Tulsa, OK. The runway 14/32 is 2,200' of very smooth sod by 60' wide. Use 122.9 (Mt Vernon's) UNICOM frequency and announce "landing at Rebel's Bluff." AV Gas 100LL will be available for approximately $2.50/gallon. Rain date is May 14th if it is a complete washout. RSVP would be greatly appreciated to your host Les Featherston at lwfeatherston(at)aol.com or call 417-466-4663 at home, or 417-425-3595 cell. Overnighters can stay at the Super 8 for $53, or camping by the creek (with flush toilet) is available. Looking forward to seeing all of you again. Les ************************************************************************ Les has a gorgeous Harmon. Pics on my pireps page if you're interested. http://www.usi.edu/science/chemistry/vfrazier/Pilot%20reports.html I plan to go to the flyin. I've been to Les's flyin previously and it was very nice. If anyone wants more info and can't reach Les, feel free to call me... 812-464-1839 M-F Vince ________________________________________________________________________________
Date: May 03, 2005
From: Paul Folbrecht <paulfolbrecht(at)yahoo.com>
Subject: Re: IO-320 in 9(A)/Catto props
Thanks for the comments, Jeff. (If you didn't recognize the name, I'm a new Ch 18 member & we chatted a bit (with Glenn) at last Tuesday's meeting.) I'd have to say that testimony goes a long way towards me buying a Catto. Since RVs are his speciality I'd be surprised if he's not at least matching Sensenich numbers. And he's even cheaper than they are. And you're right about the looks, that's for sure! I've long lusted after a three-bladed prop but thought the CS MT was about the only choice. $$$. ~Paul Folbrecht, PP-SEL-IA ~C-152 N89795, MWC ~RV-9A QB ordered > I'll second what others have written about communicating with Craig. I > just bought a prop from him (took delivery three days before leaving for > SnF) and had a lot of communication back and forth. He had computer > problems so email was out. He always answers the phone or returns calls > quickly. Very good guy to deal with. He did tell me that about 90% of > his business nowadays is making 3 blade props for RVs. > > My prop is a 3 blade Catto, 66 inch pitch and 76 inch pitch. It is on > an Aerosport Power/ Superior O-360, carb, 8.5 pistons, one mag and one > Lightspeed II ignition. Pretty stock engine. I talked with Craig at > some length about the prop pitch. I explained that I wanted a prop > which was not quite a cruise, but closer to a cruise than a climb prop. > The Sterba wood prop which it replaced (and is now on Ebay if anyone is > interested- shameless plug) was just such a prop. I was willing to > sacrifice a couple knots of top end for better short field performance. > Craig assured me that I would see an increase in top end with no loss of > acceleration or short field performance. > > Well, the proof is in the pudding. I saw about a 5 kt increase in > cruise (75%, 8K ft standard) from 172 to 177 ktas. I hit 180 ktas at > 4500 ft racing a 200HP/ Hartzell blended airfoil RV-8 (I was nose to > nose with him at full throttle for several minutes, until he pushed the > RPM up past 2400!) I saw a pretty substantial decrease in static RPM > (around 180 or so) but seem to have no loss of acceleration or takeoff > distance. I guess the prop produces more thrust at lower RPM than the > old one. As for real world cruise- around 2500 RPM gives TAS in the low > 160s with burns around 8.5-9 GPH, depending on altitude. A fixed pitch > prop just has to turn too damn fast to get real power out of the engine, > but gas is expensive and I like to baby the engine anyway. > > The prop changed the feel of the engine a lot. It now feels and sounds > more like a 6 cylinder engine than a 4 banger. I can't say it's > quieter, but it's a different, higher frequency type of noise. There > are a couple rough RPM ranges down low. Not any more so than with my > old prop, but it seems more noticable in comparison. I have yet to get > it dynamically balanced but that is in the works. > > One more thing- my wheel landings seem to have gotten better. I think > that subconsciously I am no longer worried about a prop strike with the > small diameter prop;) > > Oh, one more thing- it looks cool as hell! > > Jeff Point > RV-6 > Milwaukee WI > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Philip Condon" <pcondon(at)mitre.org>
Subject: FAA FSDO website and FAA Aircraft Certification website
Date: May 03, 2005
http://www.faa.gov/avr/afs/fsdo/index.cfm & http://www.faa.gov/certification/aircraft/av-info/dst/amateur/ambuilt_aif.ht m Flight Standards Region and Field Offices * Includes International Field Offices && You can find additional amateur-built aircraft related information by visiting the links provided above: FAA Order 8130.2, "Airworthiness Certification of Aircraft and Related Products". FAA Order 8130.33, "Designated Airworthiness Representatives: Amateur-Built and Light-Sport Aircraft Certification Functions". Advisory Circular 20-27, "Certification and Operation of Amateur-Built Aircraft". Advisory Circular 20-139, "Commercial Assistance During Construction of Amateur-Built Aircraft". Advisory Circular 21-12, "Application for U.S. Airworthiness Certificate, Form 8130-6". Advisory Circular 90-89, "Amateur-Built Aircraft and Ultralight Flight Testing Handbook". Advisory Circular 65-23, "Certification of Repairpersons (Experimental Aircraft Builders)". Advisory Circular 39-7, "Airworthiness Directives". Special Airworthiness Information Bulletins (SAIB) which may be applicable to amateur-built aircraft or to products installed on them. Related Amateur-built Aircraft Forms: AC Form 8050-88 (PDF) "Affidavit of Ownership for Amateur-Built Aircraft". FAA Form 8000-38, "Fabrication/Assembly Operation Checklist". (See Fig. 4-15 in Order 8130.2 linked above) FAA Form 8130-12 "Eligibility Statement: Amateur-Built Aircraft". FAA Form 8130-6 "Application for U.S. Airworthiness Certificate". FAA Form 8610-2, "Airman Certification and/or Rating Application". We provide an amateur-built aircraft overview page and an amateur-built registration, marking and inspection technical content page as well. The Experimental Aircraft Association (EAA) web site contains additional amateur-built information that you may find useful. As always, contact your local FAA Flight Standards District Office or Manufacturing and Inspection District Office for direct assistance in meeting your amateur-built aircraft airworthiness needs. ---- Questions about this page? Accessibility Privacy Policy For Further Information, please contact: Federal Aviation Administration Production and Airworthiness Division, AIR-200, Suite 815 800 Independence Avenue, S.W. Washington, DC 20591 Office: 202-267-8361 FAX: 202-267-5580 Page Last Updated: March 11, 2005 ________________________________________________________________________________
From: "Jerry Grimmonpre" <jerry(at)mc.net>
Subject: Re: Tip up Canopy Vs. Slider
Date: May 03, 2005
List readers ... Is the problem, of a leaking canopy, due to vent air (heated or cooling) coming in and slightly pressurizing and billowing out through the cockpit/canopy cracks? Opinions. When the ram air enters but has no outlet in the airframe, it would seem that engineering an outlet would help to keep the cockpit/canopy junctions tighter. Is there a known low pressure area on the airframe that will promote "flow through" ventilation without generating noise or allowing exhaust gases in? It seems that an engineered flow through vent system would help with the noise of escaping air around the canopy. Has anyone tried a flow through venting system? Jerry Grimmonpre Huntley IL 7a building my shop Subject: Re: RV-List: Tip up Canopy Vs. Slider > > The slider is indeed difficult to seal on the sides. Mine fits as tight as > any I've seen, but even if done perfectly there're still gaps that are > hard > to completely seal with any kind of seal material, due to the geometry > when > it opens and closes. In fact I wouldn't mind hearing from others as to how > they did that. No water comes in and I fly in the rain a fair amount, and > I > don't notice the cold air except on really cold days. But there's a fair > amount of wind noise from the gaps at the back that I just can't seam to > seal, and I'd like to get it as quiet as I can. > > Randall Henderson, RV-6 > Portland, OR > >>> >> > I would like to know if the tip up canopies seal better than the >> > sliders >> > do around the fuselage sides? I have heard that the sliders leak a >> > fair >> > amount of air around the sides of the canopy in flight. If anyone can >> > help me out with this please e-mail me. >> > >> > Robin >> > RV3B Kit 11356 >> > Minnesota >> > RMCKEE(at)MN.RR.COM ________________________________________________________________________________
From: owner-rv-list-server(at)matronics.com
Subject: Re: Long glide to landing
Date: May 03, 2005
People, just a back to basics word. IMHO, correct me if I am wrong. Here goes: Best glide rate is a function of incidence, not of speed. Best glide speed is an average. A heavily loaded plane will have a best glide speed faster than a lightly loaded plane, but the incidence will be the same. Same thing for stall - a heavily loaded plane will stall at a faster speed than a lightly loaded plane, but in both cases at an identical incidence. Air density, i.e. temperature, altitude, will also affect the best glide speed value. That is another reason for getting an AOA, which I happily have installed on my left wing. If you suddenly become a glider, get your AOA onto your best glide incidence; keep it there and forget the speed, you might gain a few hundred feet or a couple of miles. I would tend to think that the prop will have no effect on the best glide incidence. Added drag will decrease the best glide slope but it will not change the best glide incidence. This means that with an AOA, you can maximize your distance whatever the conditions. If, once you got onto your bets glide incidence you managed to time the ft/min drop and observed your speed, you'll quickly know just how far you can go before touchdown. Hope that I have not made some gross mistake - would appreciate some knowledgeable aerodynamicists to confirm this issue. And if I am correct, the above would be a compelling reason to install an AOA. Michle RV8 Fuselage > -----Original Message----- > From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list- > server(at)matronics.com] On Behalf Of gmcjetpilot(at)yahoo.com > Sent: Monday, May 02, 2005 6:52 PM > To: rv-list(at)matronics.com > Subject: RV-List: Re: Long glide to landing > > > > The effort and experimentation in glide ratio flight test is excellent, > but how will that work in an emergency. Tedd nice explanation of hi-key/ > 360 overhead approach. > > > I guess what is important to me is how can I use this info in a real > engine failure scenario. > > > "100 and 1.4" (speed 100mph and 1.4 kt mile/per thousand altitude- or 600 > ft/ NM) > > > So my first job after an engine failure/ loss of power would be get to > best glide speed (initial target speed 100mph than adjust for weight, > wind). Trim to that, while simultaneously trouble shooting engine (boost > pump, switch tanks, mixture, carb heat, ignition etc... as required) and > look for a landing spot within 1.4 kt miles per thousand feet agl. Fly the > airplane. > > > From what I got from all this that an RV will glide somewhere *10.5 to 1 > thru 8.7 to 1 ratio > > (*idle power). (Realistic engine out glide will be closer to the 8.7 to 1. > Numbers above 9 or 10 seem to be affected by partial idle power or tail > winds. A real light RV flown perfectly could do better than 8.7 to 1 but > again I am looking for something conservative I can remember and use in an > emergency, with a little margin for less than perfect speed control.) > > > Also I got best glide (max distance) is some where in the 81kt - 95 kt > range (varies with weight, altitude and head wind). Therefore I remember > 100mph (bigger mark on a/s indicator) and adjust as needed for weight. > Typical glide speed for RV best glide 84 kts = 96 mph. Min sink is under > slower. > > > Assuming engine is ka-put and I am making an emergency engine-out > glide/landing, I would assume glide ratio closer to 8. 7 to 1 than 10.5 to > 1, which sounds a little high. Therefore for every 1000 ft altitude I can > glide 1.4 kt miles (sink approx 950 ft/min or 600 ft/NM). > > > As far as windmilling prop or not, I assume the worst case, windmilling. > The most critical condition is when you have little altitude, so I would > not personally mess with trying to stop the prop. If I was at 12,000 agl > and had time I might consider it, but I would try to get the engine > running at first and keep the prop windmilling. I can't recall ever seeing > this in a POH or in training. If you think you would attempt or consider > trying to stop the prop (windmilling) in a real emergency, I would suggest > you practice it first under controlled conditions. I have not, from what I > hear is it takes near stall speed and may be even a touch of flaps? In the > time messing with all that, how much altitude do you loose vs. just going > to best glide and time lost making headway towards your intended landing > site? Also no one has real good windmill vs stopped prop numbers. There > has to be a trade off. Again unless I am real high and no chance of > getting the engine started such as catastro > phic > failure vs carb ice that might melt and allow engine to start at lower > (warmer) altitudes, than I am dubious at how practical it is. No argument > stopped is less drag. > > > Cheers George > > > Glide ratio , glide distance , power off landing > > > > > ________________________________________________________________________________
From: Wheeler North <wnorth(at)sdccd.edu>
Subject: compression testing
Date: May 03, 2005
I guess it must depend on the size/strength of the person. I have been doing them single person for over 20 years and have never had on get away from me yet. But then again I am 250 lbs and admit that I was taught from the very beginning on how to do it by myself. Mike Robertson I have a friend who has been in the industry for 30+ years. Was doing an annual on an Piper a few hangars down. He came by looking kinda shaken, with his armpit very bruised. The only two things he had to say were, "Sure glad there was a rubber boat in the hangar" and "You can see the marks of my toes dragging up the lower cowl as I went over the engine" Still does it by himself, as do I, but he pays more attention these days... W ________________________________________________________________________________
From: "Philip Condon" <pcondon(at)mitre.org>
Subject: Online FAA Forms and paperwork web site
Date: May 03, 2005
http://forms.faa.gov/forms I needed form 8610-2 and got it here. http://forms.faa.gov/forms/faa8610-2.pdf Thanks to EAA and DAS FED Mike Robertson Keywords for future electronic searching FAA paperwork forms application certificate rating applicant form online forms faa website documents ________________________________________________________________________________
Date: May 03, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: try-it-yourself fly-in - was Long glide to landing
On 22:47:16 2005-05-02 "Greg Young" <gyoung@cs-sol.com> wrote: > Slowing the aircraft > below best glide speed to stop the prop and then regaining airspeed > to best glide involves some loss of gliding range. Actually that isn't a given. I worked this out once, it seems that the break point is how high you are when you make the decision that you're landing. If you're still above your normal circuit height, there will be a net gain in gliding distance realised by stopping the prop. The reason is that when you raise the nose to stop the prop, you climb a bit above your (windmilling) ideal glide path. Once it's stopped, you may dip below the ideal (windmilling) glide path briefly while you get your airspeed up to best glide again, but the resulting new (prop stopped) glidepath will be shallower and will end up crossing the previous path well before touchdown. Now, this was worked out for a Cessna 150, and that only required slowing to 55mph or so to stop the metal prop... Which isn't much below best glide. If you've got a wooden prop, it's likely you won't need to raise the nose much to stop the prop, so you won't lose much by doing so. Still, I probably wouldn't try it unless I was over 2000' AGL, or unless I knew the second it happened that I needed every inch of gliding distance to make it to a field. > For the reasons above I don't think stopping the > prop is reasonable or even possible in many cases and therefore > objected to calling it THE realistic condition. I agree. There is never *one* answer to any situation. -Rob ________________________________________________________________________________
Date: May 03, 2005
From: "Rob Prior (rv7)" <rv7(at)b4.ca>
Subject: Re: Long glide to landing
On 7:43:39 2005-05-03 owner-rv-list-server(at)matronics.com wrote: > I would tend to think that the prop will have no effect on the best > glide incidence. Added drag will decrease the best glide slope but it > will not change the best glide incidence. AOA is a very nice insrument to have, i'm surprised that generally it's just the military that has them. They aren't particularly expensive, is there some downside to them that people don't generally talk about? And yes, you are correct. The AOA shouldn't change for best glide, but you can be sure that with the reduced drag of the windmilling prop, that you will have an increased *range* at that best glide incidence. Which means you might make it over that last farmer's fence or powerline before hitting your ideal landing spot. > Hope that I have not made some gross mistake - would appreciate some > knowledgeable aerodynamicists to confirm this issue. And if I am > correct, the above would be a compelling reason to install an AOA. Well, I did stay in a Holiday Inn Express last night... (just kidding, I did take Aeronautical Engineering as a minor in university). -Rob ________________________________________________________________________________
Subject: Hartzell service and trip report (long)
Date: May 03, 2005
From: "Frazier, Vincent A" <VFrazier(at)usi.edu>
> Guys, > > I just returned from Piqua, OH, home of Hartzell Propeller. It was a > fabulous trip. No, I don't get anything to say this stuff.... to say > that I was impressed would be a gross understatement. > > A little background first, I bought a new Hartzell two blade from Mark > for my bird. Oddly, after 22 hours it developed a minor grease leak. > Since it was still leaking 10 hours later, I thought I should check on > it. > > I called Hartzell and they said "Bring it over and we'll fix it." No > hassles, no grilling questions, no evading, no delays. They were very > accommodating of my schedule even though I told them that it was not > an emergency since I fly for fun and have no set schedule. > > I asked if we (John Crabtree went with me) could see the repair > process since we were curious (clueless, really) about what is inside > of one of these props. Not only did we get to see the overhaul > facility, we got a tour of the manufacturing facility too. More about > those later. > > I also wanted to get a dynamic balancing while I was there. WOW! > Does that make a huge difference! I didn't think my vibration level > was bad, but now it is very smooth. To say that I am pleased would > also be a gross understatement. It's worth every penny of the > approximately $180 cost.... chump change in aviation dollars. HIGHLY > RECOMMENDED regardless of what you're swinging up front. > > John and I had arranged to arrive on Sunday morning. Even though > those are not regular business hours, there were several people > around. We were greeted like we were the most important people on > earth, not like we were interrupting their weekend... which we were! > After we put the planes in the Hartzell hangar, John and I hopped in > the airport car and spent the rest of the day at the Wright-Patterson > AF museum. WPAFM is a great museum. And it's free! Where else does > the government give you anything worthwhile for FREE? > > The next morning we arrived back at the Hartzell hangar. My prop was > already well along in the repair process so after checking on it, we > hopped back into the company car and went to see one of the four > Hartzell facilities in Piqua. We went to the facility that > manufactures metal props. On the way to the facility, I got into the > wrong lane, a turn lane. A Hartzell employee on her way to work > spotted the airport car and knowing where we were supposed to be > going, motioned for us to follow her. Now, that's customer service! > > We arrived at the metal prop production facility, a state of the art > operation to say the least, and met John Popel, a tech rep. John gave > us some safety glasses and off we went. We saw everything. It was > amazing. It's simply beyond my ability to type it all. If you are > impressed by industrial equipment and appreciate the art that goes > into producing a product, this is a must-see facility. John Popel had > an amazing grasp of the minutest details and you could tell he is the > kind of guy who is excited to go to work every day. John said that > cameras were allowed in almost all areas... and wouldn't you know it, > I didn't bring one along!! DOH! John said that a facility tour can > be arranged for small groups easily. This would make a stupendous EAA > chapter event. I learned more about props in 2 hours than I have in > the last 20 years. > > While at the production facility, we also got to talk to Les Doud, a > propeller integration engineer. Les also was a wealth of useful > information. John and I asked him 500 questions. I asked if Hartzell > had a job opening for me. LOL. > > Les explained to us what to look for in a prop, what was good, and > what was bad. We tried to get some info on what products were in the > pipeline and told them that we wanted a 25# prop with better > performance... and it needed to cost less than $1000... and last > forever. Les and John had every reason to whack us on the head, but > instead simply said that they were working on it. LOL! Seriously, > after seeing the effort that they put into their prop design, > production, and service I almost felt guilty for paying as little as I > did for mine. > > Crabtree and I headed back to the airport to see how my grease leak > repair was coming along. When we arrived my prop was being rolled out > to the Rocket. We inquired what, if any, problems were found. > Everything looked OK was the reply. Mark, the lead mechanic, > explained that occasionally a grease zerk check ball will dribble a > little bit, or some of the petroleum distillates will escape from the > grease with weather changes, age, etc., or it might have simply had a > bit of stray grease get past the O-ring. I was happy to hear that > nothing was wrong. It's very comforting to have THE experts look over > your installation and say "Looks fine." > > While Mark was putting the prop back on the Rocket, John and I took > the full tour of the overhaul facility. Steve Reindel showed us > around the overhaul shop, which was a miniaturized version of the > factory, with many of the same capabilities. Steve explained that > Hartzell had overhauled their overhaul procedures, so to speak, so > that they could beat the overhaul business competition is all > categories: price, quality, and turnaround time. Seeing as how they > got my prop in and turned around in just a few hours... I believe him! > Although my prop was covered under warranty, the price Steve said I > would have paid otherwise was quite reasonable... on the order of a > few hundred dollars for the entire inspection, repair, and > reinstallation. Wow! > > In summary: > 1) Hartzell service rocks! (No, they didn't pay, coerce, or bribe me > to say it.) > 2) My teeny-weeny problem was given more attention than Air Force One > probably gets. > 3) Hartzell gives a great tour. Unbelievably informative. Highly > recommended. > 4) The cost was minimal. In airplane dollars, it was chump change for > the entire trip. > 5) My prop was inspected and installed by experts.... Priceless. > > Other trivia: > 6) Never put more than 6 pumps of grease (1 ounce) into your prop > during service, usually at annual. Use the proper grease. Make sure > you take the opposite zerk out so you don't push grease past the seal. > I didn't do any of these things since I haven't had to service my prop > yet, but it must be a common user error because we heard it mentioned > several times. > 7) We also got to go to the air force museum... too cool. If you've > never been there... why the heck not? > If you feel compelled to reply to this long message.... please SNIP out the excess! > Vince Frazier > 3965 Caborn Road > Mount Vernon, IN 47620 > 812-464-1839 work > 812-985-7309 home > F-1H Rocket, N540VF > http://www.usi.edu/science/chemistry/vfrazier/page1.html > > ________________________________________________________________________________
From: "Charles Rowbotham" <crowbotham(at)hotmail.com>
Subject: Re: Long glide to landing
Date: May 03, 2005
Michle, I absolutely agree with you on purchasing and installing an AOA. It should be the number one item on one's installation agenda. Chuck Rowbotham RV-8A >From: owner-rv-list-server(at)matronics.com >Reply-To: rv-list(at)matronics.com >To: >Subject: RE: RV-List: Re: Long glide to landing >Date: Tue, 3 May 2005 16:43:39 +0200 > > >People, just a back to basics word. IMHO, correct me if I am wrong. Here >goes: > >Best glide rate is a function of incidence, not of speed. Best glide speed >is an average. A heavily loaded plane will have a best glide speed faster >than a lightly loaded plane, but the incidence will be the same. Same thing >for stall - a heavily loaded plane will stall at a faster speed than a >lightly loaded plane, but in both cases at an identical incidence. > >Air density, i.e. temperature, altitude, will also affect the best glide >speed value. That is another reason for getting an AOA, which I happily >have >installed on my left wing. If you suddenly become a glider, get your AOA >onto your best glide incidence; keep it there and forget the speed, you >might gain a few hundred feet or a couple of miles. > >I would tend to think that the prop will have no effect on the best glide >incidence. Added drag will decrease the best glide slope but it will not >change the best glide incidence. This means that with an AOA, you can >maximize your distance whatever the conditions. If, once you got onto your >bets glide incidence you managed to time the ft/min drop and observed your >speed, you'll quickly know just how far you can go before touchdown. > >Hope that I have not made some gross mistake - would appreciate some >knowledgeable aerodynamicists to confirm this issue. And if I am correct, >the above would be a compelling reason to install an AOA. > >Michle >RV8 Fuselage ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: May 03, 2005
Subject: break in
Any one have a proven breakin for an overhauled engine? New bearings, new cylinders ect. Stewart RV-4 Co. ________________________________________________________________________________
From: "Gordon or Marge Comfort" <gcomfo(at)tc3net.com>
Subject: try-it-yourself fly-in - was Long glide to landing
Date: May 03, 2005
Subject: RE: RV-List: try-it-yourself fly-in - was Long glide to landing It seems we're really arguing the definition of "realistic." I will agree that a stopped prop represents the lowest drag configuration which in turn nets better sink and glide ratio. What I don't agree with is whether it is "realistic" (or wise) to do what it takes to get the prop stopped in any given engine out. If it occurs at 400 AGL and 80 mph I would assert that it is decidedly unwise as you'll be on the ground in 10-15 seconds. At 10,000 AGL and 170 kts you have more freedom to optimize things. Somewhere in between there's a transition point from unwise to possible to desireable. Slowing the aircraft below best glide speed to stop the prop and then regaining airspeed to best glide involves some loss of gliding range. How much and whether you can recover it with the lower drag (and how long it takes) is anyones guess. There are 4000 RVs flying and over a thousand folks on this list and I've still not seen any performance data solid enough to do that kind of trade-off study with any confidence. So we're left with our judgement to decide. My reasoning is that at low altitude (pick your own definition, 0-3K AGL?) your options are most limited and fast and correct decisions are most critical. It's not the time to approach stall in an emergency and you've got enough other things to do in the time remaining. At high altitude you may have many more options so the ability to eek out the last bit of glide range may not be that valuable. You're likely to gain more by correctly judging the effect of the wind on your range and available airports. At any event I would leave stopping the prop until after all the essentials are completed and all restart attempts are done. At that point you've lost more altitude and marginalized the benefits somewhat. My view of "realistic" is what is conservatively attainable in real world conditions. For the reasons above I don't think stopping the prop is reasonable or even possible in many cases and therefore objected to calling it THE realistic condition. It's certainly subjective so YMMV. Regardless of your view, it's important to periodically evaluate your views and practices. Regards, Greg Young - Houston (DWH) RV-6 N6GY - project Phoenix Navion N5221K - just an XXL RV-6A Greg: Good post. I have not tried to establish my RV-4's performance with the prop either stopped or windmilling but do have some anecdotes that may shed some light on what happens (or not). The first involves a 260hp Cherokee Six and its owner, my instructor. A discussion of the time required to regain power after running a tank dry resulted in a demonstration. While I was flying he moved the fuel selector to an empty tank. Presently the engine stopped producing power. The change in sound was not dramatic but was certainly perceptable. He then switched to a tank with fuel and we timed the interval until restart. My recollection is that it took 13 seconds. Seemed a long time. The engine continued to turn at governed speed and most of the 13 seconds were spent slowing down. Only a little altitude was lost near the end of the 13 seconds. The second was a forced landing exercise in my -4. We were at cruise at about 1500' AGL when the throttle (not the mixture) was pulled. Since I was busy picking a spot and setting up for an approach I did not time it but there was a lot of time available in level flight before getting down to glide speed. The third was an occasion when I was running prop performance tests. I had set up a two way course between the Davis Besse and Enrico Fermi power plants over the western end of Lake Erie. It was early in the morning and the air was as stable as it gets around here during warm weather and I was at full throttle and concentrating on holding altitude to plus or minus 10 feet when I ran a tank dry. Not very bright, I'll admit, but it happened. It took perhaps 1 second to recognize what had happened, a couple more to switch tanks and only 5 or 6 more to get power back. The throttle was not moved, no altitude was lost though there may have been a bobble when I reached for the fuel selector, and not more than 15 knots of speed were lost. Now a fourth incided occurs to me. At about 150' while climbing out of the airport in a 65 horse Aeronca Champ the instructor pulled the throttle and said "where're you gonna put it?' I dumped the stick and pointed at the biggest open space I could see. Some thoughts: If I set up speed reciprocals between those two nuclear power plants today I would expect F16's with armed missiles pretty soon. Proper response to power failure is totally dependent on height and flight conditions at the time. A fast, clean airplane at high speed provides more time to establish a course of action. If low and slow whether the prop is turning or not, while not without consequence, likely must be accepted as it is. Likewise, a slow, high drag bird like my neighbors UPF7 requires a response different from that of an RV. If you have time to experiment with stopping the prop without jeopardizing the outcome, it's your hide you're playing with. If you are high and fast and can zoom to a speed that stops the prop perhaps a better chance to succeed can be found. If you screw it up, all bets are off. Gordon Comfort N363GC ________________________________________________________________________________
From: "Ed Holyoke" <bicyclop(at)pacbell.net>
Subject: Tip up Canopy Vs. Slider
Date: May 03, 2005
On the other hand, I raised the rear pin blocks by 2 washers before I did my skirts. I removed the washers and the rear skirts were so tight that the pins wouldn't fully engage. I ended up putting the washers back under there and I'm hoping that maybe someday it'll settle enough to remove one or both of them. The skirts were fitted by the work the twist into them across a thigh method and then pulled down hard by a helper while they were drilled and clecoed. The biggest deal is having the rear of the canopy frame match the fuselage skin before hand. If it lines up right, you can make the skirts fit. If not, you'll fight it. Ed Holyoke -----Original Message----- From: owner-rv-list-server(at)matronics.com [mailto:owner-rv-list-server(at)matronics.com] On Behalf Of Doug Gray Subject: Re: RV-List: Tip up Canopy Vs. Slider > If you block up the slider during fitting and assembly of the aft skirts, > they will then fit quite nice and snug when you remove the blocks. The only > air/rain we have that leaks into the slider is the very tiny bit that comes in > around the sliding rail cap at the top due to the low pressure in this area. > One of these days I'll fashion a way to plug this area. > > IMO the slider is a pretty tight fit if done well. > > > GV (RV-6A N1GV O-360-A1A, C/S, Flying 742hrs, Silicon Valley, CA) > How high did you block the slider for this method? Also, how did you seal the side skirts? Doug Gray On approach to slider anxiety... ________________________________________________________________________________
Date: May 03, 2005
From: Mickey Coggins <mick-matronics(at)rv8.ch>
Subject: Re: Hartzell service and trip report (long)
>>AF museum. WPAFM is a great museum. And it's free! Where else does >>the government give you anything worthwhile for FREE? >> Hi Vince, I know this was "tongue-in-cheek", but if you come fly in Europe for a while, you'll be reminded of all the great stuff the government in the US is giving you for "free"! Just in case you don't have time to do this, here are a couple of items: o) Free landings at public airports (Here in Switzerland mine charges 25 USD, and each touch and go is counted!) o) Free IFR ATC services (the charging scheme in Europe is too complicated to describe, but trust me, it makes the landing fees seem cheap) So, when you read those "scare" articles from AOPA about how they are working to save us from a fee-based system, pay attention! Just about every pilot I've met is a Libertarian, but keep in mind what privatization means for your favorite pastime. Those of us flying in Europe are living it, and it ain't pretty. -- Mickey Coggins http://www.rv8.ch/ #82007 Wiring ________________________________________________________________________________
Date: May 03, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: break in
That will depend mostly on the cylinders you are using... steel, nickel, chrome etc... Any one have a proven breakin for an overhauled engine? New bearings, new cylinders ect. Stewart RV-4 Co. Darrell Reiley Round Rock, Texas RV 7A #70125 N622DR (reserved) ________________________________________________________________________________
From: "Garth Shearing" <Garth(at)islandnet.com>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
Date: May 03, 2005
Another lister gave his data on the stop prop and restart speeds for an RV. Since I haven't completed the RV6A, I haven't tried to get the data myself. Burt Rutan published the glide performance for my VariEze in the Owner's Manual showing two scenarios: 1. The engine out with prop windmilling; and 2. the engine idling. The glide ratios for these are about 10 to 1 and 17 to 1 respectively. Later on, he tested the VariEze to obtain the speeds necessary to stop the prop and to get it going again with a Continental 0-200 engine installed. These speeds were about 70 Knots and 110 Knots if I recall correctly. If your engine stops when you are close to the ground, stopping the prop is probably not an option as others have pointed out. But at 8,000 feet altitude it's a slam dunk IMHO. BTW these start and stop speeds will vary depending on actual aircraft model, engine, and propeller. When I had my Continental engine failure in my VariEze due to a seized exhaust valve, I obviously didn't have to consciously stop the prop. This occurred at about 4.5 miles from the threshold of the airport runway I just left at Victoria Intenational and I had just leveled out at 2,500 feet (airport is at 63 feet AMSL). I was still at climb speed of 120 mph. I declared an emergency and had to turn about 210 degrees to my left to establish the glide directly to the button of runway 090. The wind was about 5-10 Knots coming from my left. I immediately started looking for a place to land but soon determined that the runway was within gliding distance. When I got near the airport I actually had to purposely lose altitude. I could have used a closer runway. I landed about half way down the main active 7,000 foot runway, where I could turn off onto a taxiway to get out of the way. It turns out the gliding speed I used, about 100 mph, was about 15 mph above actual best gliding speed. Since I know pretty accurately where I was when the engine failed, I can calculate my actual gliding ratio which turns out to be something better than 10 to 1 (worst case). So optimally the engine stopped gliding ratio for the VariEze is probably about 12 to 1, or somewhat better than the prop windmilling value. An interesting side note. To be honest I can worry about a lot of things when I'm flying but when this incident occurred I had no panic at all. I just had a job to get done. I even thought I would lose it some time after I landed. That didn't happen either. The guys in the firetrucks were a lot more concerned than me. It's funny how your brain works. Some of this is off topic, but I hope it's informative. Garth Shearing VariEze & 90% RV6A Victoria BC Canada ----- Original Message ----- From: "Chris W" <1qazxsw23edcvfr45tgbnhy67ujm(at)cox.net> Subject: Re: RV-List: try-it-yourself fly-in - was Long glide to landing > <1qazxsw23edcvfr45tgbnhy67ujm(at)cox.net> > > Garth Shearing wrote: > >> >>And I beg to differ with you, Greg. If you want minimum sink rate, low >>drag, and maximum distance to glide, you have to reduce speed to stop the >>prop, and then increase speed to best glide ratio. In the unlikely event >>that the best glide ratio speed restarts the windmilling, then use a >>slightly lower glide speed. In an engine out emergency, that is the >>realistic and best condition. >> >>Don't ask me how I know. >> >> >> > How slow did you have to go to get the prop to stop? While I agree that > it would be best to stop the prop and then go to best glide speed, if > you are say less than 3000 ft AGL, don't you think there would be too > little time to do that? Once I get my ticket and build my -7, I don't > ever plan on being much less than 8,000 ft AGL except for takeoff & > landing, very short trips and when crossing mountain peaks. In my part > of the country 8,000 ft AGL isn't hard to do and with that much room, if > the engine quits, you generally have at least 2 airports with in gliding > range. > > -- > Chris W ________________________________________________________________________________
Date: May 03, 2005
From: <gmcjetpilot(at)yahoo.com>
Subject: Re: Long glide to landing
>Doug wrote: >I asked the pilot what the rate of decent was power off in his airplane. He said, "I don't >know, I suppose around 500 fpm." I said we would go up over the airport and pull the >mixture and find out. He was concerned about that. I asked him why? He said "What if >it doesn't restart?" We land, I replied. If anyone is concerned in the least about an engine >failure at 3000 AGL directly over a 6500 x 250 ft runway they should not be flying single >engine airplanes. >If you are not comfortable shutting down your engine over an airport, find a >flight instructor and go do it ASAP. Unfortunately most flight instructors are teaching to >gain experience rather than share it. If your flight instructor is unwilling to do it, find a >different flight instructor. Doug: The pilot in command is the pilot getting the BFR. The instructor giving a BFR to a current pilot is not the PIC. When he said to you, "What if the engine does not start?" that was a very valid question. What if cut-off is used in training and the engine does not come back in time or at all? The FAA would rightly blame the CFI. I think CFIs should provide realistic training with out undue risk to the student or yourself. Doug if you feel it is safe, that is your judgment call, but I respectively disagree with your suggestion that a CFI who does not use idle cutoff is unworthy some how to teach. You don't have to simulate an emergency with a real emergency. Regardless what is under you at the time, loss of power, intentional or not, in a single engine airplane is always an emergency. Pulling mixture in flight has risks. Not sure what you are advocating, but if you are suggesting dead stick landing practice with the mixture in cut-off, I would say that is unnecessarily risky, and I know if an accident resulted the FAA would agree. I agree at 3000 feet over a long runway and engine failure should be no problem. However what if? Vehicle on runway, you miss judge and the engine wont fire up? It has happened. If you are alluding to simulating engine out glide, in a single engine airplane, with partial power and flaps. That is a great idea. However you demonstrated glide performance by actually using idle cutoff? Why? Could you not just tell the pilot what the best glide ROD-rate of decent is and appropriate speed, without shutting the engine down? BTW 900-1000 fpm @ 96 kts is a good number for most RVs (1.4 to 1.6 nm/1000ft). I know it is not as macho, and the law of INTENSITY says making it "real" enhances learning but not if the student is scared. It sounds like you took that into consideration and explained this. I would say just tell the student what to expect from experience without demonstrating it with idle cutoff, and simulate using partial flaps at idle power as you apparently did. Again great idea. I would say anyone who has a CFI that says you must practice with idle cut-off, whether at high altitude or low, go find another CFI, If you are not comfortable with it. Even going to idle power has some risks, like carb ice, thus CFIs check or clear the engine occasionally. In defense of Doug he apparently he has supreme confidence in making a dead stick landing and limits the risk by practice over a runway, but is that extra risk for realistic training needed? It is not common to use idle cutoff and some would say, including the FAA, not necessary. In the early days of multi-engine training, engine failures were simulated with with idle cutoff mixture. Many accidents resulted from this practice. Engine failures on takoff and landing for multi-engine airplanes are now simulated with idle power (per the FAA PTS-practical test standards). Feathering the engine is done by using simulated with "zero thrust and partial power. I would say that is a good conservative approach to carry over the SE airplanes. Regards George CFI(CFII)(MEI), ATP +++++++++++++++++++++++++++++++++++++++++++++ From: "Doug Rozendaal" <dougr(at)petroblend.com> Subject: Re: try-it-yourself fly-in - was Long glide to landing Date: May 01, 2005 I was giving a BFR this week and I asked the pilot what the rate of decent was power off in his airplane. He said, "I don't know, I suppose around 500 fpm." I said we would go up over the airport and pull the mixture and find out. He was concerned about that. I asked him why? He said "What if it doesn't restart?" We land, I replied. If anyone is concerned in the least about an engine failure at 3000 AGL directly over a 6500 x 250 ft runway they should not be flying single engineairplanes. We pulled the mixture and flew best glide speed and the airplane came down 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. We found that 1/3 flaps and idle thrust simlated that decent, then we practiced deadstick overhead 360 and 180 approaches to a specific point on the runway, without going short. He did well and I would suspect his chances of successfully making a deadstick landing increased dramatically. If you are not comfortable shutting down your engine over an airport, find a flight instructor and go do it ASAP.Unfortunately most flight instructors are teaching to gain experience ratherbthan share it. If your flight instructor is unwilling to do it, find a different flight instructor. A successful outcome from a bad situation is directly related to the confidence the pilot has in that outcome. If you have realistically trained for, and successfully completed deadstick landings on a point, you will have a much higher level of confidence in the outcome and that increases the likelyhood of a successful outcome WHEN (not if) the fire goes out. Tailwinds,Doug Rozendaal ________________________________________________________________________________
From: "cgalley" <cgalley(at)qcbc.org>
Subject: Re: Fuel Senders
Date: May 03, 2005
Sounds like you are going beyond the full position and the wiper is hanging on the edge of the resistor. Probably will not happen in the wing. Cy Galley - Bellanca Champion Club Newsletter Editor-in-Chief & EAA TC www.bellanca-championclub.com Actively supporting Bellancas every day ----- Original Message ----- From: "Vincent Welch" <welchvincent(at)hotmail.com> Subject: RV-List: Fuel Senders > > Gentlemen, > > I am having a problem with my SW fuel senders. It seems that the floats > are > sticking at the pivot point. I removed the units and I can move the floats > by > hand but when I lift the float to the full position and release it, it > remains. If I shake or jiggle it, the float will drop. Is there some way > to > free up the mechanism? I am afraid that as I burn fuel, the sender won't > follow the level. > > Any ideas? > > Vince > RV-8A > > > ________________________________________________________________________________
Date: May 03, 2005
From: Hal Kempthorne <hal_kempthorne(at)sbcglobal.net>
Subject: Re: compression checking an engine
Yeah. Area on top of piston is about 20 sqin, length of stroke about 6 80 * 20 * 6 = 9600 lbs/in torque on crankshaft 36 inches to the tip of the prop 9600 / 36 = 270 in lbs at the tip = 22 ft lbs. Easy to hold but if your grip slips and the force can change from static to dynamic then run! You might be able to stand on the flap (static) but don't jump up and down (dynamic). I like to have a helper. hal ________________________________________________________________________________
Date: May 03, 2005
From: <chaztuna(at)adelphia.net>
Subject: Re: compression checking an engine
Hal Your numbers are a bit off. The stroke of an O-320 is 3.875". The 360 has a stroke of 4.375" (not 6") Charlie Kuss ---- Hal Kempthorne wrote: > > Yeah. Area on top of piston is about 20 sqin, length of stroke about 6 > > 80 * 20 * 6 = 9600 lbs/in torque on crankshaft > > 36 inches to the tip of the prop > > 9600 / 36 = 270 in lbs at the tip = 22 ft lbs. > > Easy to hold but if your grip slips and the force can change from static to dynamic then run! > > You might be able to stand on the flap (static) but don't jump up and down (dynamic). > > I like to have a helper. > > hal > > > > > > ________________________________________________________________________________
Date: May 03, 2005
From: Kevin Horton <khorton01(at)rogers.com>
Subject: Re: Long glide to landing
> >You don't have to simulate an emergency with a real emergency. >Regardless what is under you at the time, loss of power, intentional >or not, in a single engine airplane is always an emergency. Pulling >mixture in flight has risks. Not sure what you are advocating, but >if you are suggesting dead stick landing practice with the mixture >in cut-off, I would say that is unnecessarily risky, and I know if >an accident resulted the FAA would agree. I agree at 3000 feet over >a long runway and engine failure should be no problem. However what >if? Vehicle on runway, you miss judge and the engine wont fire up? >It has happened. > >If you are alluding to simulating engine out glide, in a single >engine airplane, with partial power and flaps. That is a great idea. >However you demonstrated glide performance by actually using idle >cutoff? Why? Could you not just tell the pilot what the best glide >ROD-rate of decent is and appropriate speed, without shutting the >engine down? BTW 900-1000 fpm @ 96 kts is a good number for most RVs >(1.4 to 1.6 nm/1000ft). Given that every RV is a bit different (different ASI errors, different VSI errors, different prop pitch, or low pitch stop setting for a CS prop), how is one to determine what partial power and flap combination properly simulates engine out unless you perform an actual engine-out glide first? The parametres that properly simulate an engine-out glide in one RV may be completely out to lunch in another one. -- Kevin Horton RV-8 (finishing kit) Ottawa, Canada http://www.kilohotel.com/rv8 ________________________________________________________________________________
From: "D Paul Deits" <pdeits(at)comcast.net>
Subject: Wiring diagram
Date: May 03, 2005
Earlier this year either as a result of a list entry or reviewing a lister's site, I reviewed a well thought out wiring diagram. I have misplaced my copy. Anyone remember the site etc.? ________________________________________________________________________________
From: "Kyle Boatright" <kboatright1(at)comcast.net>
Subject: Re: Tip up Canopy Vs. Slider
Date: May 03, 2005
On the RV-6, there is a low pressure area along the side canopy skirts. This is because the fuselage begins to narrow about 1/2 way back along the skirts, and because that area also coincides with the low pressure area above the wing. Flow through ventilation is the problem - air is sucked into the cockpit through every other orifice in the airplane and exhausts around the side skirts. You can cut a piece of foam pipe insulation in half and place it between the slider tracks and the slider skirt to seal the area in flight. I carry a couple of pieces of this stuff with me during cool weather, and it makes a huge difference in the amount of cold air blowing through the cockpit. Adding more "exit" air ventilation would only make the problem worse. KB ----- Original Message ----- From: "Jerry Grimmonpre" <jerry(at)mc.net> Subject: Re: RV-List: Tip up Canopy Vs. Slider > > List readers ... > Is the problem, of a leaking canopy, due to vent air (heated or cooling) > coming in and slightly pressurizing and billowing out through the > cockpit/canopy cracks? > > Opinions. > > When the ram air enters but has no outlet in the airframe, it would seem > that engineering an outlet would help to keep the cockpit/canopy junctions > tighter. > > Is there a known low pressure area on the airframe that will promote "flow > through" ventilation without generating noise or allowing exhaust gases > in? > It seems that an engineered flow through vent system would help with the > noise of escaping air around the canopy. > > Has anyone tried a flow through venting system? > Jerry Grimmonpre > Huntley IL 7a building my shop > > Subject: Re: RV-List: Tip up Canopy Vs. Slider > ________________________________________________________________________________
From: "Vic Jacko" <vicwj(at)earthlink.net>
Subject: Re: Fuel Senders
Date: May 03, 2005
----- Original Message ----- From: "cgalley" <cgalley(at)qcbc.org> Subject: Re: RV-List: Fuel Senders > > Sounds like you are going beyond the full position and the wiper is > hanging > on the edge of the resistor. Probably will not happen in the wing. > > Cy Galley - Bellanca Champion Club > Newsletter Editor-in-Chief & EAA TC > www.bellanca-championclub.com > Actively supporting Bellancas every day > > > ----- Original Message ----- > From: "Vincent Welch" <welchvincent(at)hotmail.com> > To: > Subject: RV-List: Fuel Senders > > >> >> Gentlemen, >> >> I am having a problem with my SW fuel senders. It seems that the floats >> are >> sticking at the pivot point. I removed the units and I can move the >> floats >> by >> hand but when I lift the float to the full position and release it, it >> remains. If I shake or jiggle it, the float will drop. Is there some way >> to >> free up the mechanism? I am afraid that as I burn fuel, the sender won't >> follow the level. >> >> Any ideas? >> >> Vince >> RV-8A >> >> >> > > > ________________________________________________________________________________
From: "Vic Jacko" <vicwj(at)earthlink.net>
Subject: Re: Fuel Senders
Date: May 03, 2005
I will wager the sloshing of the fuel will do what you are doing when you shake or jiggle it! Vic ----- Original Message ----- From: "cgalley" <cgalley(at)qcbc.org> Subject: Re: RV-List: Fuel Senders > > Sounds like you are going beyond the full position and the wiper is > hanging > on the edge of the resistor. Probably will not happen in the wing. > > Cy Galley - Bellanca Champion Club > Newsletter Editor-in-Chief & EAA TC > www.bellanca-championclub.com > Actively supporting Bellancas every day > > > ----- Original Message ----- > From: "Vincent Welch" <welchvincent(at)hotmail.com> > To: > Subject: RV-List: Fuel Senders > > >> >> Gentlemen, >> >> I am having a problem with my SW fuel senders. It seems that the floats >> are >> sticking at the pivot point. I removed the units and I can move the >> floats >> by >> hand but when I lift the float to the full position and release it, it >> remains. If I shake or jiggle it, the float will drop. Is there some way >> to >> free up the mechanism? I am afraid that as I burn fuel, the sender won't >> follow the level. >> >> Any ideas? >> >> Vince >> RV-8A >> >> >> > > > ________________________________________________________________________________
From: "Darwin N. Barrie" <ktlkrn(at)cox.net>
Subject: Andair fuel valve/Gascolator FS
Date: May 03, 2005
Hi All, I have a NIB Andair gascolator with 3/8" female fittings and quick drain valve for sale. $185 (Spruce price $189.95 + 29.95) Also, New mounted but never used Andair FS20-20-D2 fuel selector valve. This has female fittings, 3/8" feed, 1/4" return. $380. $550 for both + shipping I'm changing directions and don't need these for my set up. Darwin N. Barrie P19 ________________________________________________________________________________
From: RVer273sb(at)aol.com
Date: May 03, 2005
Subject: Re: break in
That would be mellenium for the cylinders. Nitrided steel I believe. Thanks, Stewart ________________________________________________________________________________
From: "Jerry Huether" <huether(at)charter.net>
Subject: Hangar space needed (wanted?) June 16-23 at KBRD
Date: May 03, 2005
Anyone have space for an RV6 at KBRD or nearby from June 16-23 for rent? DNA Jerry Huether RV-6 Tualatin, OR ________________________________________________________________________________
Date: May 03, 2005
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Fuel Senders
If you fly a Lyc, you've got nothing to worry about... Charlie ;-) cgalley wrote: > >Sounds like you are going beyond the full position and the wiper is hanging >on the edge of the resistor. Probably will not happen in the wing. > >Cy Galley - Bellanca Champion Club > Newsletter Editor-in-Chief & EAA TC > www.bellanca-championclub.com > Actively supporting Bellancas every day > > >----- Original Message ----- >From: "Vincent Welch" <welchvincent(at)hotmail.com> >To: >Subject: RV-List: Fuel Senders > > > > >> >>Gentlemen, >> >>I am having a problem with my SW fuel senders. It seems that the floats >>are >>sticking at the pivot point. I removed the units and I can move the floats >>by >>hand but when I lift the float to the full position and release it, it >>remains. If I shake or jiggle it, the float will drop. Is there some way >>to >>free up the mechanism? I am afraid that as I burn fuel, the sender won't >>follow the level. >> >>Any ideas? >> >>Vince >>RV-8A >> ________________________________________________________________________________
Date: May 03, 2005
From: Darrell Reiley <lifeofreiley2003(at)yahoo.com>
Subject: Re: break in
Search this off of yahoo... http://www.avweb.com/news/maint/182895-1.html Should help... Darrell RVer273sb(at)aol.com wrote: That would be mellenium for the cylinders. Nitrided steel I believe. Thanks, Stewart ________________________________________________________________________________
From: "Paul Rice" <rice737(at)msn.com>
Subject: Landing Lights
Date: May 03, 2005
Hey All, I was at Sun and Fun and saw that many of you have those small landing lights in the wing tips. They look like the type Vans sell for the RV-10, but vans says they will not work in the RV-8 wing tips, the parts person said they are to hot and would melt the tip. Where would I find what I saw in many planes at the airshow. I want to install them in the wing tip with the strobe and the nav. light. Thanks. Paul ________________________________________________________________________________
From: Fiveonepw(at)aol.com
Date: May 03, 2005
Subject: Re: Landing Lights
In a message dated 05/03/2005 7:31:31 PM Central Standard Time, rice737(at)msn.com writes: I was at Sun and Fun and saw that many of you have those small landing lights in the wing tips. >>> Hi Paul- These are the ones I used- http://www.autobarn.net/helopperdriv.html 55w each, which after a number of night landings I would say are "adequate" just not outstanding. (sure wish I could find some 75w bulbs!) They offer a really nice beam, fairly tight with enough to the sides to see the runway edges well. The oval shape nests nicely into the outer curve of the newer style tips. Got mine at the AutoZone or Advance Auto Parts, don't remember which, but do a Google on "Optilux 1500" and you'll get a bunch of hits... I also recessed my nav/strobe fixtures the depth of the baseplate for less blanking of the main lights- I'll send a foto. Mark Phillips ________________________________________________________________________________
From: "Evan and Megan Johnson" <evmeg(at)snowcrest.net>
Subject: Re: Fuel Senders
Date: May 03, 2005
If they are not new you may have some sticky units....I have handled a lot of these and the older the units (even if they have never been installed) the stickier they tend to be. If they are really hanging up just chuck them in favor of some new units. The wise on the list will remind you that you should never count on the sender/instrument being accurate anyway.....I agree, but why not at least try to have them close. My 2 cents.... Evan Johnson www.evansaviationproducts.com (530)247-0375 (530)351-1776 cell ----- Original Message ----- From: "Vincent Welch" <welchvincent(at)hotmail.com> Subject: RV-List: Fuel Senders > > Gentlemen, > > I am having a problem with my SW fuel senders. It seems that the floats are > sticking at the pivot point. I removed the units and I can move the floats > by > hand but when I lift the float to the full position and release it, it > remains. If I shake or jiggle it, the float will drop. Is there some way to > free up the mechanism? I am afraid that as I burn fuel, the sender won't > follow the level. > > Any ideas? > > Vince > RV-8A > > ________________________________________________________________________________
From: "George Inman" <ghinman(at)mts.net>
Subject: Manifold pressure to primer port
Date: May 03, 2005
What did others use to connect Manifold press. to primer port Primer fittings are 5/16 32 but some say to use AN816-4 Whch is 1/4 inch The primer port on my #4 cyl. seems a bit larger than 1/4" GEORGE H. INMAN ghinman(at)mts.net CELL 204 799 7062 HOME 204 287 8334 ________________________________________________________________________________
From: "LarryRobertHelming" <lhelming(at)sigecom.net>
Subject: Re: break in
Date: May 03, 2005
Suggest you use Google to search for "Lycoming break in" That will find you several hits including this one http://www.lycoming.textron.com/main.jsp?bodyPage=/support/publications/keyReprints/operation/engineBreakIn.html Indiana Larry, RV7 Tip Up FLYING - Phase 1 Testing 1 hr done, 39 to go. Much Fun, what work....... ----- Original Message ----- From: "Darrell Reiley" <lifeofreiley2003(at)yahoo.com> Subject: Re: RV-List: break in > > Search this off of yahoo... http://www.avweb.com/news/maint/182895-1.html > > Should help... > > Darrell > > RVer273sb(at)aol.com wrote: > > That would be mellenium for the cylinders. > Nitrided steel I believe. > Thanks, > Stewart > > > ________________________________________________________________________________
Date: May 03, 2005
From: "Richard E. Tasker" <retasker(at)optonline.net>
Subject: Re: Landing Lights
This is probably what you saw (although I wasn't at SnF this year). http://www.creativair.com/cva/index.php?cPath=21 Dick Tasker Paul Rice wrote: > >Hey All, > >I was at Sun and Fun and saw that many of you have those small landing >lights in the wing tips. They look like the type Vans sell for the RV-10, >but vans says they will not work in the RV-8 wing tips, the parts person >said they are to hot and would melt the tip. Where would I find what I saw >in many planes at the airshow. I want to install them in the wing tip with >the strobe and the nav. light. >Thanks. >Paul > > > > -- ---- Please Note: No trees were destroyed in the sending of this message. We do concede, however, that a significant number of electrons may have been temporarily inconvenienced. ---- ________________________________________________________________________________
From: "Doug Rozendaal" <dougr(at)petroblend.com>
Subject: Re: Long glide to landing
Date: May 03, 2005
George, Thank you for your well thought out post. You make several good points and it is clear we disagree. I do not want to argue your post point by point. My thesis is this. I believe we have dumbed down training to accommodate the low experience level of the instructors doing the training and the result is dumber pilots. I take a FAR 61.58 checkride every year in something, sometimes twice a year, and the FAA requires (Per the ATP PTS) we do a shutdown, feather, and restart, every time. I guess the FAA assumes that if you fly a large (read over 12,500#) airplane you need more "realistic" training. I can assure you that I am much better for that training/checking. The airplane I was flying for the BFR in my post was a homebuilt and the pilot had no idea of the sink rate and there was no book to look in. I have done this with several pilots and based on my experience, the learning that occurs far outweighs the risk. And you are absolutely correct, the risk is mine! With regard to the risk the mixture cable is exactly the same type of cable that controls the throttle and if it failing is the concern it is exactly the same risk as the throttle. If the carb is the concern, the chances of a throttle butterfly getting jammed are far greater than the mixture needle valve getting jammed. I fly 60 year old airplanes every weekend. Pulling the mixture over a 3000 feet over 6500 foot runway is a risk I can live with. I see pilots who have learned to fly and successfully passed FAA checkrides, and yet have no concept of how fast an airplane comes down and I continue to see pilots who think they can turn back from an engine failure at 500 feet and land on the runway they departed from. I am also a FAR 135 check airmen for the local Charter service. Recently we had a Seneca that had runout engines. We lined up all the Charter pilots, some are long in the tooth, gray haired, or no haired types. We went up high over the airport and shut one down and flew around on it. I do quite a bit of training, and I can recognize when learning occurs. Learning occurred. These guys got to see for real what single engine performance was really like. Not simulated, not numbers on a page, but numbers on a barely climbing altimeter in a lightly loaded Seneca. They got to see the importance of raising the dead and splitting the ball. Learning occurred. The restarts were a real eye-opener. One of the pilots had recently had a precautionary shutdown for an oil pressure problem and he considered a restart for landing. After a real restart, he said, "if I had tried to restart when I planned, I would have never made the airport." Learning occurred. Is there risk associated with that type of training? You bet. Is there reward? Absolutely. Can the risk be mitigated? I think so. Many ways. A through briefing. Flying at altitudes that if the other engines quits we still would have landed on the airport. The risk associated with a shutdown, feather, and restart in a B-25 is probably 100 fold greater than pulling the mixture in a light single engine airplane over a runway. I believe the current state of flight training is terrible. I believe flight instructors should be required to have 1000's of hours not a few hundred. I believe instructors should be paid similar to other corporate or airline pilots. (I am not, and do not want to be a full time flight instructor, even if the pay was better) In short I believe there are lots and lots of pilots out there who do not have a clue about the airplanes they are flying, on several subjects, engine failures are one, but there is one pilot in Iowa who has a better understanding, and I believe it was worth the risk. But then you could find several people who would say I am one of the clueless ones ;-) Tailwinds, Doug Rozendaal ----- Original Message ----- From: <gmcjetpilot(at)yahoo.com> Subject: RV-List: Re: Long glide to landing > > > >Doug wrote: > > >I asked the pilot what the rate of decent was power off in his airplane. He said, "I don't >know, I suppose around 500 fpm." I said we would go up over the airport and pull the >mixture and find out. He was concerned about that. I asked him why? He said "What if >it doesn't restart?" We land, I replied. If anyone is concerned in the least about an engine >failure at 3000 AGL directly over a 6500 x 250 ft runway they should not be flying single >engine airplanes. > > > >If you are not comfortable shutting down your engine over an airport, find a > >flight instructor and go do it ASAP. Unfortunately most flight instructors are teaching to >gain experience rather than share it. If your flight instructor is unwilling to do it, find a > >different flight instructor. > > > Doug: > > > The pilot in command is the pilot getting the BFR. The instructor giving a BFR to a current pilot is not the PIC. When he said to you, "What if the engine does not start?" that was a very valid question. > > > What if cut-off is used in training and the engine does not come back in time or at all? The FAA would rightly blame the CFI. I think CFIs should provide realistic training with out undue risk to the student or yourself. Doug if you feel it is safe, that is your judgment call, but I respectively disagree with your suggestion that a CFI who does not use idle cutoff is unworthy some how to teach. > > > You don't have to simulate an emergency with a real emergency. Regardless what is under you at the time, loss of power, intentional or not, in a single engine airplane is always an emergency. Pulling mixture in flight has risks. Not sure what you are advocating, but if you are suggesting dead stick landing practice with the mixture in cut-off, I would say that is unnecessarily risky, and I know if an accident resulted the FAA would agree. I agree at 3000 feet over a long runway and engine failure should be no problem. However what if? Vehicle on runway, you miss judge and the engine wont fire up? It has happened. > > > If you are alluding to simulating engine out glide, in a single engine airplane, with partial power and flaps. That is a great idea. However you demonstrated glide performance by actually using idle cutoff? Why? Could you not just tell the pilot what the best glide ROD-rate of decent is and appropriate speed, without shutting the engine down? BTW 900-1000 fpm @ 96 kts is a good number for most RVs (1.4 to 1.6 nm/1000ft). > > > I know it is not as macho, and the law of INTENSITY says making it "real" enhances learning but not if the student is scared. It sounds like you took that into consideration and explained this. I would say just tell the student what to expect from experience without demonstrating it with idle cutoff, and simulate using partial flaps at idle power as you apparently did. Again great idea. > > > I would say anyone who has a CFI that says you must practice with idle cut-off, whether at high altitude or low, go find another CFI, If you are not comfortable with it. Even going to idle power has some risks, like carb ice, thus CFIs check or clear the engine occasionally. > > > In defense of Doug he apparently he has supreme confidence in making a dead stick landing and limits the risk by practice over a runway, but is that extra risk for realistic training needed? It is not common to use idle cutoff and some would say, including the FAA, not necessary. In the early days of multi-engine training, engine failures were simulated with with idle cutoff mixture. Many accidents resulted from this practice. Engine failures on takoff and landing for multi-engine airplanes are now simulated with idle power (per the FAA PTS-practical test standards). Feathering the engine is done by using simulated with "zero thrust and partial power. I would say that is a good conservative approach to carry over the SE airplanes. > > > Regards George CFI(CFII)(MEI), ATP > > > +++++++++++++++++++++++++++++++++++++++++++++ > > From: "Doug Rozendaal" <dougr(at)petroblend.com> Subject: Re: try-it-yourself fly-in - was Long glide to landing Date: May 01, 2005 > > > I was giving a BFR this week and I asked the pilot what the rate of decent > was power off in his airplane. He said, "I don't know, I suppose around 500 > fpm." I said we would go up over the airport and pull the mixture and find > out. He was concerned about that. I asked him why? He said "What if it > doesn't restart?" We land, I replied. If anyone is concerned in the least about an engine failure at 3000 AGL directly over a 6500 x 250 ft runway they should not be flying single engineairplanes. > > > We pulled the mixture and flew best glide speed and the airplane came down > 1000 fpm measured on my watch, not the VSI. The VSI showed about 800 fpm. We > found that 1/3 flaps and idle thrust simlated that decent, then we practiced > deadstick overhead 360 and 180 approaches to a specific point on the runway, > without going short. He did well and I would suspect his chances of > successfully making a deadstick landing increased dramatically. > > If you are not comfortable shutting down your engine over an airport, find a > flight instructor and go do it ASAP.Unfortunately most flight instructors are teaching to gain experience ratherbthan share it. If your flight instructor is unwilling to do it, find a > different flight instructor. > > > A successful outcome from a bad situation is directly related to the > confidence the pilot has in that outcome. If you have realistically trained > for, and successfully completed deadstick landings on a point, you will have > a much higher level of confidence in the outcome and that increases the > likelyhood of a successful outcome WHEN (not if) the fire goes out. > > Tailwinds,Doug Rozendaal > > ________________________________________________________________________________
From: "Bill VonDane" <bill(at)vondane.com>
Subject: Re: Landing Lights
Date: May 03, 2005
www.creativair.com ----- Original Message ----- From: "Paul Rice" <rice737(at)msn.com> Subject: RV-List: Landing Lights Hey All, I was at Sun and Fun and saw that many of you have those small landing lights in the wing tips. They look like the type Vans sell for the RV-10, but vans says they will not work in the RV-8 wing tips, the parts person said they are to hot and would melt the tip. Where would I find what I saw in many planes at the airshow. I want to install them in the wing tip with the strobe and the nav. light. Thanks. Paul ________________________________________________________________________________
Date: May 04, 2005
From: Doug Gray <dgra1233(at)bigpond.net.au>
Subject: Re: try-it-yourself fly-in - was Long glide to landing
So does best glide speed differ between 'prop windmilling' and 'prop stopped' glide? And if so, by how much? Doug Gray ________________________________________________________________________________
From: "Charles Heathco" <cheathco(at)comcast.net>
Subject: Re: try-it-yourself fly-in - was Long glide to landingtry-it-yourself
fly-in - was Long glide to landing
Date: May 04, 2005
I was told to run it pedal to the metal for 1 1/2 to 2 hrs continuous. Result in good normal consumption breakin. (O-320e2a) As an aside, I have gottien advice to only use 100LL, that use of Mogas is bad for breakin. However, I have not seen any compelling data re this. If it is due to the myth that LL suplies some


April 24, 2005 - May 04, 2005

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