RV-List Digest Archive

Mon 03/21/05


Total Messages Posted: 41



Today's Message Index:
----------------------
 
     1. 12:07 AM - Re: Whelan Wingtip Strobe Cover Removable? (Sterling)
     2. 03:36 AM - RV-4 for sale (Jorge Gonzalez)
     3. 05:55 AM - Re: Greasy flap motors, cont'd (Hopperdhh@aol.com)
     4. 06:03 AM - Re: Greasy flap motors, cont'd (Hopperdhh@aol.com)
     5. 06:15 AM - Capacitance Fuel sender instructions (Eric Parlow)
     6. 06:20 AM - Re: cockpit noise abatement? (Hopperdhh@aol.com)
     7. 06:39 AM - Re: Greasy flap motors, cont'd (Oliver Washburn)
     8. 06:40 AM - Intermediate Canopy Latch - RV4 (Derrick Aubuchon)
     9. 06:41 AM - Re: Capacitance Fuel sender instructions (Paul Trotter)
    10. 06:42 AM - Re: Failure on Motion Control actuators used on Experimental Aircraf... (Hopperdhh@aol.com)
    11. 06:45 AM - Re: Greasy flap motors, cont'd (Hopperdhh@aol.com)
    12. 06:49 AM - Re: Bar-BQ fly-in Mar. 26- Fl Wing VAF (Charles Heathco)
    13. 07:01 AM - Re: Capacitance Fuel sender instructions (Evan and Megan Johnson)
    14. 08:09 AM - Re: Strobe Lighting (James H Nelson)
    15. 08:56 AM - Wing incidence (Bob Hodgson)
    16. 09:38 AM - Re: Strobe Lighting (Bill VonDane)
    17. 09:46 AM - Re: Wing incidence (Bob J)
    18. 09:49 AM - Re: Wing incidence (Bob J)
    19. 09:56 AM - Tech Counselor in FtWorth area? (RV Builder (Michael Sausen))
    20. 10:04 AM - Re: Greasy flap motors, cont'd (HCRV6@aol.com)
    21. 10:13 AM - Re: Greasy flap motors, cont'd  (Jerry2DT@aol.com)
    22. 10:37 AM - Positioning Main Gear Inflation Holes (DAVID REEL)
    23. 11:26 AM - E-mag (sportav8r@aol.com)
    24. 12:48 PM - Re: Wing incidence (randall)
    25. 12:51 PM - Re: Positioning Main Gear Inflation Holes (randall)
    26. 12:57 PM - Re: Prop replacement, question for Das Fed, was: (Travis Hamblen)
    27. 01:47 PM - Re: Bar-BQ fly-in Mar. 26- Fl Wing VAF (Oliver Washburn)
    28. 01:53 PM - Re: Wing incidence (Bob J)
    29. 02:01 PM - Re: Prop replacement, question for Das Fed, was: (Ed Anderson)
    30. 02:12 PM - Orndorf videos for sale, $1.00 (Sterling)
    31. 02:31 PM - Re: Prop replacement, question for Das Fed, was: (Charlie England)
    32. 02:36 PM - Re: E-mag (RVer273sb@aol.com)
    33. 03:15 PM - Another $1.00 Orndorf Video on Ebay (Sterling)
    34. 04:17 PM - Re: Prop replacement, question for Das Fed, was: (Ed Anderson)
    35. 04:52 PM - AILERON TRIM SPRINGS (Jsd41@aol.com)
    36. 05:30 PM - Re: AILERON TRIM SPRINGS (Ed Anderson)
    37. 05:45 PM - Re: AILERON TRIM SPRINGS (Hopperdhh@aol.com)
    38. 06:09 PM - Re: AILERON TRIM SPRINGS (Jim Oke)
    39. 06:15 PM - Re: AILERON TRIM SPRINGS (Pat Hatch)
    40. 09:46 PM - Canopy Breaker Survival Gear ()
    41. 11:05 PM - Re: Prop replacement, question for Das Fed, was: (Mickey Coggins)
 
 
 


Message 1


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    Time: 12:07:26 AM PST US
    From: "Sterling" <sterling@pgrb.com>
    Subject: Re: Whelan Wingtip Strobe Cover Removable?
    --> RV-List message posted by: "Sterling" <sterling@pgrb.com> Easily removable with one screw. Very easy to break when it comes out of the aluminum housing, so be prepared to catch it when you pull the aluminum housing off. If you drop it and it breaks, it isn't easy on the wallet. If you do break it, I'll sell you my spare at 1/2 of what Aircraft Spruce gets. ----- Original Message ----- From: <tx_jayhawk@excite.com> Subject: RV-List: Whelan Wingtip Strobe Cover Removable? > --> RV-List message posted by: "" <tx_jayhawk@excite.com> > > All, Stupid question...is the clear glass cover over the strobe flashtube on the wingtip combo lights (Whelan) removable? Thanks,Scott > >


    Message 2


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    Time: 03:36:39 AM PST US
    From: Jorge Gonzalez <jetpilot@powercruising.com>
    Subject: RV-4 for sale
    --> RV-List message posted by: Jorge Gonzalez <jetpilot@powercruising.com> I'm selling my RV-4 with 310 hours Total time Airframe and engine SOH. Details and pictures are at www.barnstormers.com. I've just retired and can't afford so many toys. Regards, Jorge Gonzalez


    Message 3


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    Time: 05:55:17 AM PST US
    From: Hopperdhh@aol.com
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: Hopperdhh@aol.com GV, I'm tempted by your offer. Hopefully, someone with an extra actuator will take you up on it. The thing is -- I have wiped away the evidence. I think it will probably return, though. Someone already has to know exactly what the problem is. After all, it has been fixed hasn't it? Come on Van, give us a hint. You can't be making that much money selling flap actuators. The bad thing about just ordering a new one is, how do I know they won't send me one just like I have? My feeling is that the problem is due to the type of lubricant used in the gearbox, or possibly the small ball bearing on the commutator end of the shaft. For example: Lubriplate is very bad about "creeping." If that is the case we could take the motor (and gearbox this time) apart again, clean it really well, and repack it with a different grease. The question is: what grease? I'll bet Motion Systems Corp. knows what we should use. I may try to call them today. First I'll call Vans and raise hell -- er, that is, ask them what could be the problem. Again, the motor was made by Motion Systems Corp. Eatontown, NJ. The label on the motor reads: 9234C120-R7 73633 12 VDC 08-21-01 Dan Hopper Walton, IN RV-7A In a message dated 3/20/05 10:24:38 P.M. US Eastern Standard Time, Vanremog@aol.com writes: Van's standard Motion Systems Corp. actuator works fine, lasts a long time since day one on my bird. With some of these Pittman motors lasting thousands of hours and some lasting only tens of hours, there must be more to the story here. I would love to look at a someone's failed motor and see if I can do the failure analysis and craft an easy fix. Any takers? GV (RV-6A N1GV O-360-A1A, C/S, Flying 736hrs, Silicon Valley, CA)


    Message 4


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    Time: 06:03:46 AM PST US
    From: Hopperdhh@aol.com
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: Hopperdhh@aol.com Stein, Thanks for your great reply. Seems like it should be possible to pinpoint the exact nature of the problem, and let us fix it, so we would not have to go through all this. As has been stated, if it were a certified plane there would have been an AD and a recall. It is not Vans fault that he was shipped some "inferior" product, but it is his fault that he didn't force the manufacturer to stand behind it. do not archive Thanks again, Dan Hopper Walton, IN RV-7A (Flying 70 hours, now in the paint shop for a while) --> RV-List message posted by: "Stein Bruch" <stein@steinair.com> Yep! Just to re-iterate what a bunch of us went through some time ago. As stated before, my final cure (as well as others) was to s!@#$can the old one and buy a new one. Van's knows all about this. No need to waste a bunch of time by anyone doing "failure analysis", etc... as Van's has already done it. The fact is, Van's received a "batch"/Lot of flap motors that were inferior in some details. I'll past the quote from the Van's letter directly below: ============================================================================ =========== "In 2002 we switched suppliers, replacing the units we'd received from Motion Systems with a custom made unit powered by a Pittman brand motor. The new units can be identified by the Van's logo incised on the aluminum gear box housing. Not long after the change was made, we got a significant number of complaints about motors failing after just a few hours. Naturally, we suspected the new motors...but as it turns out, the newer "Van's" units were not the culprit. Instead, the problem seems to appear in one of the last batches of Motion Systems units. These were received about three years ago and they are now starting to appear in finished airplanes. The problem is usually caused by an excess of grease in the gearbox... As the unit spins, hydraulic pressure pushes grease back into the motor unit and coats the windings, commutator and brushes". ============================================================================ ============= Sorry for my sarcasm on this subject, but I was one of the lucky guys who got burnt on both my RV6's with the same "bad batch" motor. Looks like problem is solved now, but in my next airplane, guess what?...the ole' johnson bar in between the seats will guarantee I'll never have this problem again! Cheers, Stein. do not archive - the complete letter as quoted above is on van's website


    Message 5


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    Time: 06:15:50 AM PST US
    From: "Eric Parlow" <ericparlow@hotmail.com>
    Subject: Capacitance Fuel sender instructions
    --> RV-List message posted by: "Eric Parlow" <ericparlow@hotmail.com> We're building a RV-8 fuel tank with capacitance fuel senders. The capacitance sensor kit is second hand and did not come with instructions. Could some tell us were to go to get the instruction or fax/scan them to us? Thanks ERic- RV-8 wings/tanks


    Message 6


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    Time: 06:20:00 AM PST US
    From: Hopperdhh@aol.com
    Subject: Re: cockpit noise abatement?
    --> RV-List message posted by: Hopperdhh@aol.com Lucky, Not noise related, but does relate to some of your post: Abby at Flightline Interiors sells the pushrod boots for the fuselage at the wing roots. It would be easier to install them with the wings off. Dan Hopper RV-7A In a message dated 3/20/05 9:24:18 P.M. US Eastern Standard Time, luckymacy@comcast.net writes: This is probably a stretch but has anyone actually done a before and after type test on adding one of the *popular* heat/noise abatement materials onto the firewall? I've ridden in a few different RVs of various makes and they were all loud and were hot or cold depending on what the outside was doing. Can't recall my feet in a side by side being influenced by firewall temp. Some were all decked out in leather and filled in panels everywhere and some were plain. I didn't seem to notice the difference. My hunch is closing off the big fuse holes like ailerons and such will probably help the most but now is the time for me to finish off the firewall barrier if I do it at all. thx, lucky


    Message 7


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    Time: 06:39:06 AM PST US
    From: "Oliver Washburn" <ollie6a@earthlink.net>
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: "Oliver Washburn" <ollie6a@earthlink.net> I think that in almost cases when an AD is issued against an aircraft it is up to the owner to pay for it. Ollie 6a > --> RV-List message posted by: Hopperdhh@aol.com > > > Stein, > > Thanks for your great reply. Seems like it should be possible to > pinpoint > the exact nature of the problem, and let us fix it, so we would not have > to go > through all this. As has been stated, if it were a certified plane there > would have been an AD and a recall. It is not Vans fault that he was > shipped > some "inferior" product, but it is his fault that he didn't force the > manufacturer to stand behind it. > > do not archive > > Thanks again, > > Dan Hopper > Walton, IN > RV-7A (Flying 70 hours, now in the paint shop for a while) > > > --> RV-List message posted by: "Stein Bruch" <stein@steinair.com> > > Yep! > > Just to re-iterate what a bunch of us went through some time ago. As > stated > before, my final cure (as well as others) was to s!@#$can the old one and > buy a new one. > > Van's knows all about this. No need to waste a bunch of time by anyone > doing "failure analysis", etc... as Van's has already done it. The fact > is, Van's received a "batch"/Lot of flap motors that were inferior in > some > details. I'll past the quote from the Van's letter directly below: > > ============================================================================ > =========== > "In 2002 we switched suppliers, replacing the units we'd received from > Motion Systems with a custom made unit powered by a Pittman brand motor. > The new units can be identified by the Van's logo incised on the aluminum > gear box housing. Not long after the change was made, we got a > significant > number of complaints about motors failing after just a few hours. > > Naturally, we suspected the new motors...but as it turns out, the newer > "Van's" units were not the culprit. > > Instead, the problem seems to appear in one of the last batches of Motion > Systems units. These were received about three years ago and they are > now > starting to appear in finished airplanes. The problem is usually caused > by > an excess of grease in the gearbox... > > As the unit spins, hydraulic pressure pushes grease back into the motor > unit > and coats the windings, commutator and brushes". > ============================================================================ > ============= > > Sorry for my sarcasm on this subject, but I was one of the lucky guys who > got burnt on both my RV6's with the same "bad batch" motor. Looks like > problem is solved now, but in my next airplane, guess what?...the ole' > johnson bar in between the seats will guarantee I'll never have this > problem > again! > > Cheers, > Stein. > > do not archive - the complete letter as quoted above is on van's website > > >


    Message 8


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    Time: 06:40:23 AM PST US
    From: Derrick Aubuchon <n184da@volcano.net>
    Subject: Intermediate Canopy Latch - RV4
    --> RV-List message posted by: Derrick Aubuchon <n184da@volcano.net> Greetings Listers, Well, after 400hrs, I decided that it's finally time to install an intermediate canopy latch on my RV4,, not wishing to spend another summer sweltering on the taxiway. I have seen several variations of the latches over the years, and I am requesting from my fellow listers,, any photos that they might have available of whatever is working for their birds. I think the "coolest" design I had seen was one that I believe was originally developed by the Bakersfield gang,, using an over-center type latch mounted on the roll bar,, I remember that there used to be some drawings related to that type of latch,,?? But any ideas will be appreciated. Thanks,, Derrick L. Aubuchon RV-4: N184DA Jackson/Westover -Amador County (O70) n184da@volcano.net


    Message 9


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    Time: 06:41:57 AM PST US
    From: Paul Trotter <ptrotter@acm.org>
    Subject: Re: Capacitance Fuel sender instructions
    --> RV-List message posted by: Paul Trotter <ptrotter@acm.org> Eric, I'd be happy to fax you the instructions, but you may also need the drawing page which is the same size as the rest of Van's drawings. I could probably get that copied and mail it to you if you like. Email me offline and we can make arrangements. Paul ----- Original Message ----- From: "Eric Parlow" <ericparlow@hotmail.com> Subject: RV-List: Capacitance Fuel sender instructions > --> RV-List message posted by: "Eric Parlow" <ericparlow@hotmail.com> > > We're building a RV-8 fuel tank with capacitance fuel senders. > > The capacitance sensor kit is second hand and did not come with > instructions. > > Could some tell us were to go to get the instruction or fax/scan them to us? > > Thanks > ERic- > RV-8 wings/tanks > >


    Message 10


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    Time: 06:42:36 AM PST US
    From: Hopperdhh@aol.com
    Subject: Re: Failure on Motion Control actuators used on Experimental
    Aircraf... --> RV-List message posted by: Hopperdhh@aol.com Gary, Did you send this post to Motion? Let me make some clarifications. In my case (that you quoted below) I wouldn't call it a lack of grease. It looked like the motor was as it should have been, except for the grease or oil on the commutator and brushes. Also, see my earlier post about being able to make the motor run by just touching the motor shaft. (This is not possible to do with the covers over the flap mechanism in the aircraft.) The grease may have "creeped" out of the ball bearing near the commutator, or down the motor shaft from the gearbox. I didn't open up the gearbox end of the motor. There was however some small amount of grease bulging out of a couple of holes (screw holes?) into the motor from the gearbox. I used a cotton swab to remove this grease from the motor side. One thing that may be contributing to these failures is the mounting position of the actuator. The motor is at the top, but the assembly leans back about 30 degrees from vertical making the commutator end of the motor lower than the gearbox. Nowhere on the motor does it say Pittman, so I'm not sure of the brand. If no one else volunteers their actuator within a few days, you can have mine. My airplane is down for at least 2 months anyway. It is in the paint shop, and we can't rush this guy! Dan Hopper Walton, IN RV-7A In a message dated 3/20/05 10:48:36 P.M. US Eastern Standard Time, Vanremog@aol.com writes: Gentlemen- I am affiliated with a national group of pilots building a series of aircraft kits made by Van's Aircraft. This aircraft uses your actuator and there have been some failures related to the Pittman motor used therein. Below is the text is a letter recently received on our forum, that highlights the problem in general. I am a Mechanical Engineer working in the Defense Industry and my primary interest with our group is to find out how to prevent the problems that some of our builders are experiencing and ultimately to help make these aircraft as mechanically safe and reliable as they can be. I have your product in my plane and it works very well over the past 7 yrs, but some are having repeated failures over just short periods of operation. ================================Start of text of supporting posting I removed the brush end of the motor and found almost NO grease in the motor, except on the brushes. The commutator was black with oil that wiped right off. I cleaned it up with a clean rag, cleaned the brushes with alcohol, and put it back together. I won't be able to fly the airplane for about 2 months, so you won't know for a while how long it lasted. I don't know where the oil came from. Maybe its from the little ball bearing race. BTW, I was able to use some #28 insulated copper wire to wire the brush springs back during reassembly. In case anyone needs this information, the motor was made by Motion Systems Corp. Eatontown, NJ. The label on the motor reads: 9234C120-R7 73633 12 VDC 08-21-01 ===============================End of text of supporting posting I have offered to receive any motor actuator to try to understand how they are failing, but apparently many builders just give up and switch to a manual system rather than pursue a remedy. Reports indicate that excessive (and in some rare cases, lack of) lubricating grease is contributing to these problems. I would like to engage you in helping to identify and remedy these issues. Thank you in advance and please advise. Gary VanRemortel (RV-6A N1GV O-360-A1A, C/S, Flying 736hrs, Silicon Valley, CA)


    Message 11


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    Time: 06:45:37 AM PST US
    From: Hopperdhh@aol.com
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: Hopperdhh@aol.com Ollie, Aw, darn. Actually, I think you're right. Dan do not archive In a message dated 3/21/05 9:40:09 A.M. US Eastern Standard Time, ollie6a@earthlink.net writes: I think that in almost cases when an AD is issued against an aircraft it is up to the owner to pay for it. Ollie 6a


    Message 12


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    Time: 06:49:27 AM PST US
    From: "Charles Heathco" <cheathco@comcast.net>
    Subject: Re: Bar-BQ fly-in Mar. 26- Fl Wing VAF
    --> RV-List message posted by: "Charles Heathco" <cheathco@comcast.net> llie, Im entering loves landing in 296, what is runw num and lenth, and elev? charlie ----- Original Message ----- From: "Oliver Washburn" <ollie6a@earthlink.net> Subject: RV-List: Bar-BQ fly-in Mar. 26- Fl Wing VAF --> RV-List message posted by: "Oliver Washburn" <ollie6a@earthlink.net> ATTENTION ALL---Mark your calendars now for one of the best fly-in Bar-BQ lunch in the Southeast. We will be serving lunch at noon and there will be coffee and donuts for the early birds.There is no rain date so come rain or shine, hopefully shine. Place----- Loves Landing Airpark, 97FL 130* 21.5 nm from Ocala VOR N 28*57.42 W 081*53.29 What----- Smoked Bar-BQ pork (takes 2 days), Hamburgers,Hotdogs and all the other fixns. When---- Lunch at noon and coffee & donuts for early birds Price---- $6.00 donation which includes everything Note---This is a private airpark, land at your own risk. Ollie Washburn 6A


    Message 13


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    Time: 07:01:55 AM PST US
    From: "Evan and Megan Johnson" <evmeg@snowcrest.net>
    Subject: Re: Capacitance Fuel sender instructions
    --> RV-List message posted by: "Evan and Megan Johnson" <evmeg@snowcrest.net> Send me your address Eric....I believe I have an extra set of drawings for this. I have installed a ton of these now and its no big deal....just takes time. Evan Johnson www.evansaviationproducts.com (530)247-0375 (530)351-1776 cell ----- Original Message ----- From: "Eric Parlow" <ericparlow@hotmail.com> Subject: RV-List: Capacitance Fuel sender instructions > --> RV-List message posted by: "Eric Parlow" <ericparlow@hotmail.com> > > We're building a RV-8 fuel tank with capacitance fuel senders. > > The capacitance sensor kit is second hand and did not come with > instructions. > > Could some tell us were to go to get the instruction or fax/scan them to us? > > Thanks > ERic- > RV-8 wings/tanks > >


    Message 14


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    Time: 08:09:47 AM PST US
    Subject: Re: Strobe Lighting
    From: James H Nelson <rv9jim@juno.com>
    --> RV-List message posted by: James H Nelson <rv9jim@juno.com> Charles, I received your answer to the Nova supplier but lost the info. Would you please send me it again. I found the Weilan system far to expensive. Jim Nelson N599RV (res)


    Message 15


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    Time: 08:56:00 AM PST US
    From: "Bob Hodgson" <bob@hodgson252.freeserve.co.uk>
    Subject: Wing incidence
    --> RV-List message posted by: "Bob Hodgson" <bob@hodgson252.freeserve.co.uk> Hi all, Question: How much difference in wing incidence did you end up with, and what difference did it make to the roll trim ?? I'm drilling / reaming the rear spar attach on my RV3B, and have read the info in Van's FAQs and RV-List archives. I did this as carefully as I knew how, but now find a difference of maybe 0.1 - 0.2 deg between the wings has crept in somehow. The right wing attach bolt is now fitted, and the left attach hole is drilled to 6 mm, just needing final reaming to 0.246 inch. Edge distances all good (mostly 5/8 inch, and min allowable on a -3 is 1/2 inch). I know this difference doesn't sound much, and checking the wings with a simple bubble level shows only a barely detectable difference. However the digital level does show a definite fraction of a degree difference. Rather than try to fix it, possibly with an oversize bolt which will compromise edge distance, do you think this amount of asymmetry will make much difference to the trim? (Some back-of-the-envelope calcs are trying to tell me there will be a roll moment of 300 lbs/ft at 180 kts . . . ). How much difference is acceptable generally before you go out of the range that can be dealt with by adjusting the flaps 'up' position, squeezing ailerons, etc? I do want this aeroplane to fly straight, but am I being paranoid here? Thanks in advance. Bob (UK)


    Message 16


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    Time: 09:38:54 AM PST US
    From: "Bill VonDane" <bill@vondane.com>
    Subject: Re: Strobe Lighting
    --> RV-List message posted by: "Bill VonDane" <bill@vondane.com> www.creativair.com ----- Original Message ----- From: "James H Nelson" <rv9jim@juno.com> Subject: Re: RV-List: Strobe Lighting > --> RV-List message posted by: James H Nelson <rv9jim@juno.com> > > Charles, > I received your answer to the Nova supplier but lost the info. > Would you please send me it again. I found the Weilan system far to > expensive. > > Jim Nelson > N599RV (res) > > > > > > >


    Message 17


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    Time: 09:46:29 AM PST US
    From: Bob J <rocketbob@gmail.com>
    Subject: Re: Wing incidence
    --> RV-List message posted by: Bob J <rocketbob@gmail.com> On Mon, 21 Mar 2005 16:55:12 -0000, Bob Hodgson <bob@hodgson252.freeserve.co.uk> wrote: > --> RV-List message posted by: "Bob Hodgson" <bob@hodgson252.freeserve.co.uk> > > Hi all, > > Question: > How much difference in wing incidence did you end up with, and what > difference did it make to the roll trim ?? No you're not being paranoid. A friend of mine who just flew his F1 for the first time in December initially drilled the rear spar for 1/4" bolts so that some adjustment could be made after the first flight. That turned out to be a good move. With the right wing being heavy he bumped the rear spar up to reduce the incidence, bumping it up nearly 1/16", then drilled it 5/16". Flew it and found that the left wing felt twice as heavy as the right wing was initially. He then bumped that wing up 1/32" and drilled it 5/16". The next flight it flew hands off and straight. While flying formation I verified sighting down the TE of both wings, all the control surfaces and wingtips are in perfect alignment. I hope to get mine dialed in that well. Regards, Bob Japundza RV-6 flying F1 under const.


    Message 18


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    Time: 09:49:16 AM PST US
    From: Bob J <rocketbob@gmail.com>
    Subject: Re: Wing incidence
    --> RV-List message posted by: Bob J <rocketbob@gmail.com> Ooops, upon re-reading my message after hitting the send button I need to clarify that he bumped up the left wing to fix the right wing heavy condition and vise versa. Regards, Bob Japundza RV-6 flying F1 under const. On Mon, 21 Mar 2005 12:45:43 -0500, Bob J <rocketbob@gmail.com> wrote: > On Mon, 21 Mar 2005 16:55:12 -0000, Bob Hodgson > <bob@hodgson252.freeserve.co.uk> wrote: > > --> RV-List message posted by: "Bob Hodgson" <bob@hodgson252.freeserve.co.uk> > > > > Hi all, > > > > Question: > > How much difference in wing incidence did you end up with, and what > > difference did it make to the roll trim ?? > > No you're not being paranoid. A friend of mine who just flew his F1 > for the first time in December initially drilled the rear spar for > 1/4" bolts so that some adjustment could be made after the first > flight. That turned out to be a good move. With the right wing being > heavy he bumped the rear spar up to reduce the incidence, bumping it > up nearly 1/16", then drilled it 5/16". Flew it and found that the > left wing felt twice as heavy as the right wing was initially. He then > bumped that wing up 1/32" and drilled it 5/16". The next flight it > flew hands off and straight. While flying formation I verified > sighting down the TE of both wings, all the control surfaces and > wingtips are in perfect alignment. > > I hope to get mine dialed in that well. > > Regards, > Bob Japundza > RV-6 flying F1 under const. >


    Message 19


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    Time: 09:56:26 AM PST US
    Subject: Tech Counselor in FtWorth area?
    From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net>
    --> RV-List message posted by: "RV Builder (Michael Sausen)" <rvbuilder@Sausen.net> Can anyone recommend a EAA Tech Counselor in the South FtWorth area that knows RV construction? I live about 30 minutes south of the I20 & 35W interchange right off of 35W (Grandview) and I'm looking for a TC. Thanks, Michael Sausen


    Message 20


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    Time: 10:04:28 AM PST US
    From: HCRV6@aol.com
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: HCRV6@aol.com In a message dated 3/20/05 4:36:45 PM Pacific Standard Time, Hopperdhh@aol.com writes: << Is there a "permanent" fix? >> Dan: I don't know about "permanent," but I thoroughly cleaned the motor parts with lacquer thinner, small brush and Q Tips. Then I used a small piece of Scotch Brite to polish the commutator and cleaned it again with solvent in a sprayer. I removed all but a small amount of grease from the worm screw in the gear box and lightly greased the screw threads on the motor shaft. Now there is no grease in the motor assembly and a small amount in the gear box. With so little grease to begin with I am confident that mine should be good for several hundred hours at least. Harry Crosby Pleasanton, California RV-6 N16CX, 45+ hours.


    Message 21


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    Time: 10:13:34 AM PST US
    From: Jerry2DT@aol.com
    Subject: Re: Greasy flap motors, cont'd
    --> RV-List message posted by: Jerry2DT@aol.com We suffered two failures on our Motion Systems motor, at around 100 and 200 hrs. First time I called MS, talked to an "engineer" who claimed they never heard of such a thing... This would have been around 12/2003. Van's laughed and said Motion Systems had been well aware of the problem. Second time I took motor over to Van's and nice fella there exchanged same, so it has been done. Don't want to get anyone in trouble so won't mention person's name. I just think if you holler enough, you'll get an exchange, and it's only right. YMMV... Jerry Cochran Wilsonville OR Time: 10:38:32 PM PST US From: "Edward Cole" <edwardmcole@comcast.net> Subject: RE: RV-List: Greasy flap motors, cont'd --> RV-List message posted by: "Edward Cole" <edwardmcole@comcast.net> I don't understand why everyone is content to put up with this failure. This has been occurring for years. There would certainly be an AD if this was a certified aircraft. If this was happening in your newly purchased vehicle or any other consumer item we'd be having a fit. The vendor should be recalling these and repairing/replacing the motors. The first time someone tries a go around with full flaps that won't retract and stuffs it in the ground, I'll bet the problem will get fixed real fast.


    Message 22


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    Time: 10:37:58 AM PST US
    From: "DAVID REEL" <dreel@cox.net>
    Subject: Positioning Main Gear Inflation Holes
    --> RV-List message posted by: "DAVID REEL" <dreel@cox.net> I'm positioning inflation holes in my RV8A main gear wheel pants so I won't have to remove the wheel pants to inflate the tire. I noticed that the valve stems for the Aero Classic TR-67 inner tubes supplied in my finish kit angle in towards the axis of the wheel so that I can just barely get the valve stem cap on without interference from the wheel hub. Do others have this same sort of angle on the valve stem? I'm imagining I get the holes bored in my wheel pants and then change to Michelin air stop tubes for example & find the valve stems exit straight out instead of at an angle making my inflation hole useless. Dave Reel - RV8A


    Message 23


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    Time: 11:26:25 AM PST US
    From: sportav8r@aol.com
    Subject: E-mag
    --> RV-List message posted by: sportav8r@aol.com The latest from Brad at Emagair today: shipping delay for the latest batch of units is estimated at 4 weeks from now. (A month ago it was "5 weeks"). Since the units are slated to arrive at the same time as Sun-N-Fun, it "wouldn't be fair" to the customers waiting for the units to delay shipping while they were off in Florida exhibiting, so don't look for an Emag booth at S-N-F unless they change their minds. I heard a disturbing rumor this weekend, while lunching with some RV buds, that this company was possibly in some financial trouble. I must admit, the phone conversation today was vague enough to be considered non-reassuring, but I will resist rumor-mongering while the events of the next few weeks speak for themselves. Obviously, as a deposit-paying customer, I very much want Emagair to succeed and to remain in business for a long time after my units are installed and flying. I had really hoped to see them in person in Lakeland next month. More that the safety of my $100 investment, I want the features of the product itself in my plane... Here's hoping! -Stormy


    Message 24


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    Time: 12:48:34 PM PST US
    From: "randall" <rv6n6r@comcast.net>
    Subject: Re: Wing incidence
    --> RV-List message posted by: "randall" <rv6n6r@comcast.net> Can you clarify whether or not he did the simple tried-and-true aileron-tweak before he changed the wing incidence? It takes SUCH a small aileron surface "bulge" to create a "heavy" wing, and such a small tweak to fix it. Seems like overkill to me to go playing with wing incidence, unless the wings are known to be out of alignment. Randall Henderson RV-6 ----- Original Message ----- From: "Bob J" <rocketbob@gmail.com> Subject: Re: RV-List: Wing incidence > --> RV-List message posted by: Bob J <rocketbob@gmail.com> > > Ooops, upon re-reading my message after hitting the send button I need > to clarify that he bumped up the left wing to fix the right wing heavy > condition and vise versa. > > Regards, > Bob Japundza > RV-6 flying F1 under const. > > On Mon, 21 Mar 2005 12:45:43 -0500, Bob J <rocketbob@gmail.com> wrote: > > On Mon, 21 Mar 2005 16:55:12 -0000, Bob Hodgson > > <bob@hodgson252.freeserve.co.uk> wrote: > > > --> RV-List message posted by: "Bob Hodgson" <bob@hodgson252.freeserve.co.uk> > > > > > > Hi all, > > > > > > Question: > > > How much difference in wing incidence did you end up with, and what > > > difference did it make to the roll trim ?? > > > > No you're not being paranoid. A friend of mine who just flew his F1 > > for the first time in December initially drilled the rear spar for > > 1/4" bolts so that some adjustment could be made after the first > > flight. That turned out to be a good move. With the right wing being > > heavy he bumped the rear spar up to reduce the incidence, bumping it > > up nearly 1/16", then drilled it 5/16". Flew it and found that the > > left wing felt twice as heavy as the right wing was initially. He then > > bumped that wing up 1/32" and drilled it 5/16". The next flight it > > flew hands off and straight. While flying formation I verified > > sighting down the TE of both wings, all the control surfaces and > > wingtips are in perfect alignment. > > > > I hope to get mine dialed in that well. > > > > Regards, > > Bob Japundza > > RV-6 flying F1 under const. > > > >


    Message 25


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    Time: 12:51:56 PM PST US
    From: "randall" <rv6n6r@comcast.net>
    Subject: Re: Positioning Main Gear Inflation Holes
    --> RV-List message posted by: "randall" <rv6n6r@comcast.net> The 1" holes in my '6 wheelpants have so far been big enough for me to use for three different brands of tire (Aero Trainers, Condors and Michelin Air). The valve stem is flexible enough that you can make it work even if its not exactly centered. Randall Henderson RV-6


    Message 26


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    Time: 12:57:21 PM PST US
    From: "Travis Hamblen" <TravisHamblen@cox.net>
    <dwight@openweave.org>, <TravisHamblen@cox.net>
    Subject: Re: Prop replacement, question for Das Fed, was:
    --> RV-List message posted by: "Travis Hamblen" <TravisHamblen@cox.net> Sorry for the late reply... I'm about 10 days behind on the list reading right now, and this is not meant as a personal stab at anyone, just the facts. I just wanted to set straight all the misconceptions about experimental aircraft maintenance. It is shocking to me that people have such misconceptions about experimental maintenance. First, if you don't have the repairman certificate for the aircraft in question then you must have an A&P sign off on the annual conditional inspection (it DOES NOT have to be an IA). Second, ANYONE can work on an experimental aircraft, major mods or alterations included. Just make sure you read the operating limitations, most state that you have to "notify" the FAA of your alterations before doing them. That means you notify them, not ask permission. Read the below pasted letter from the EAA about this matter, it should set the matter straight for any doubters out there. If you still doubt me, e-mail me and I'll send you a copy of the entire letter and you can take it to your local FSDO to confirm. This is one of the BEST things about an experimental; it sidesteps the evil empire (FAA) on most matters. With all this said, I would warn you not to do anything to an airplane that you aren't expertly trained in doing, it just may kill you or someone else! READ ON (not written by me): ** "FAR Part 43.1 (b) specifically excludes experimental aircraft so the FAA is incorrect in stating you are held to any part or appendix of Part 43. It states "This part does not apply to any aircraft for which an experimental airworthiness certificate has been issued, unless a different kind of airworthiness certificate had been previously issued for that aircraft". I stress the word aircraft so that is not interpreted to include an engine. What about major repairs and alterations? First you never have to fill out a form 337 for an experimental aircraft. Repairs major or minor can be done by anyone, remember Part 43.1 (b). However, alterations are different. If you alter the aircraft with a different propeller or engine, for example, then it is not the aircraft for which you received an airworthiness certificate. This would also apply to changing pistons or magnetos. It is a new and untested airplane. If you change propellers you must notify the FAA (not by a 337) of your change. Your aircraft's operating limitations should have a statement such as the following in regard to major changes: "The FAA Cognizant Flight Standards Office must be notified, and their response received in writing, prior to flying this aircraft after incorporating a major change as defined by FAR 21.93 If you do not have such a statement on your operating limitations then you can claim you do not have to notify the FAA. However, EAA suggest you do so even if you do not have this limitation. The FAA inspector will make a determination as to whether he need to come out and inspect the change and/or assign a new flight-test period. If the inspector gives you an OK by letter (which is often done) you should note the date, time, name and change in your aircraft logbook. If the inspector wants to inspect the aircraft, it is the same as an FAA certified A&P. So far to EAA's knowledge this has never happened on an amateur built aircraft. Most operating limitations contain a statement that says and annual "condition" inspection must be performed per the scope and detail of FAR Part 43 Appendix D. It also states that an FAA certificated A&P or repairman must perform this inspection. Note it says "A&P or Repairman". It does not require an IA. Let me clarify this. Anyone can work on an experimental aircraft and sign off the work. However the annual "condition" inspection must be completed by an A&P or a repairman. Sincerely, Experimental Aircraft Association Earl Lawrence Government Programs Specialist" *** Hope that straightens out a bunch of misunderstood maintenance issues, Travis RV-6A @ VGT RV-7A wiring (in the garage) > gmcjetpilot@yahoo.com wrote: > >>--> RV-List message posted by: <gmcjetpilot@yahoo.com> >> >> >>Mike: >> >>You are opening a can of worms :- ) The buyer of an experimental aircraft >>can only do routine maintenance, as if it were a Piper or Cessna, as far >>as I know. Only the manufacture (builder/repairman) can make major mods, >>however I assume(?) an A&P or AI could do it and with the FAA's blessing. >>Again, as in all these matters refer to the FISDO of choice for the >>answer. There is no "type certificate" configuration for exp a/c, so many >>changes slip thru the cracks and are not tracked by the FAA. Anyone who >>has a second hand RV may find them self in a regulatory mess if they want >>to make a major changes. The best (easiest) thing would get the builder to >>sign the mod off if possible. However that is one of the fantastic reasons >>for building your own plane. >> >>Cheers George ---


    Message 27


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    Time: 01:47:47 PM PST US
    From: "Oliver Washburn" <ollie6a@earthlink.net>
    Subject: Re: Bar-BQ fly-in Mar. 26- Fl Wing VAF
    --> RV-List message posted by: "Oliver Washburn" <ollie6a@earthlink.net> Charlie---Runway length is 3700' and is N-S Go to http://www.airnav.com/airports/ and type in 97FL. Gives you all info you'd ever need. Ollie ----- Original Message ----- From: "Charles Heathco" <cheathco@comcast.net> Subject: Re: RV-List: Bar-BQ fly-in Mar. 26- Fl Wing VAF > --> RV-List message posted by: "Charles Heathco" <cheathco@comcast.net> > > llie, Im entering loves landing in 296, what is runw num and lenth, and > elev? charlie > ----- Original Message ----- > From: "Oliver Washburn" <ollie6a@earthlink.net> > To: <rv-list@matronics.com> > Subject: RV-List: Bar-BQ fly-in Mar. 26- Fl Wing VAF > > > --> RV-List message posted by: "Oliver Washburn" <ollie6a@earthlink.net> > > ATTENTION ALL---Mark your calendars now for one of the best fly-in Bar-BQ > lunch in the Southeast. We will be serving lunch at noon and there will > be > coffee and donuts for the early birds.There is no rain date so come rain > or > shine, hopefully shine. > > Place----- Loves Landing Airpark, 97FL 130* 21.5 nm from Ocala VOR > N 28*57.42 W 081*53.29 > > What----- Smoked Bar-BQ pork (takes 2 days), Hamburgers,Hotdogs and all > the > other fixns. > > When---- Lunch at noon and coffee & donuts for early birds > > Price---- $6.00 donation which includes everything > > Note---This is a private airpark, land at your own risk. > > Ollie Washburn 6A > > >


    Message 28


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    Time: 01:53:21 PM PST US
    From: Bob J <rocketbob@gmail.com>
    Subject: Re: Wing incidence
    --> RV-List message posted by: Bob J <rocketbob@gmail.com> No, he was trying to avoid doing that. The incidence change was done to preserve the light aileron forces by not squeezing the light aileron, which in effect makes the ailerons heavier in feel. Overkill? Maybe, unless your really picky about handling characteristics. I do agree its simple to squeeze the ailerons, but all that may do is cover up the symptoms of a mis-rigged airplane. What this excercise did prove is that a slight change in incidence can have a big impact on a wing-heavy condition, and likely there's no way for one to get that sort of accuracy with a level when rigging the airplane. And its for that reason that many other airplanes have mechanisms to adjust incidence. Regards, Bob Japundza RV-6 flying F1 under const. On Mon, 21 Mar 2005 12:49:07 -0800, randall <rv6n6r@comcast.net> wrote: > --> RV-List message posted by: "randall" <rv6n6r@comcast.net> > > Can you clarify whether or not he did the simple tried-and-true > aileron-tweak before he changed the wing incidence? It takes SUCH a small > aileron surface "bulge" to create a "heavy" wing, and such a small tweak to > fix it. Seems like overkill to me to go playing with wing incidence, unless > the wings are known to be out of alignment. > > Randall Henderson > RV-6 > > ----- Original Message ----- > From: "Bob J" <rocketbob@gmail.com> > To: <rv-list@matronics.com> > Subject: Re: RV-List: Wing incidence > > > --> RV-List message posted by: Bob J <rocketbob@gmail.com> > > > > Ooops, upon re-reading my message after hitting the send button I need > > to clarify that he bumped up the left wing to fix the right wing heavy > > condition and vise versa. > > > > Regards, > > Bob Japundza > > RV-6 flying F1 under const. > > > > On Mon, 21 Mar 2005 12:45:43 -0500, Bob J <rocketbob@gmail.com> wrote: > > > On Mon, 21 Mar 2005 16:55:12 -0000, Bob Hodgson > > > <bob@hodgson252.freeserve.co.uk> wrote: > > > > --> RV-List message posted by: "Bob Hodgson" > <bob@hodgson252.freeserve.co.uk> > > > > > > > > Hi all, > > > > > > > > Question: > > > > How much difference in wing incidence did you end up with, and what > > > > difference did it make to the roll trim ?? > > > > > > No you're not being paranoid. A friend of mine who just flew his F1 > > > for the first time in December initially drilled the rear spar for > > > 1/4" bolts so that some adjustment could be made after the first > > > flight. That turned out to be a good move. With the right wing being > > > heavy he bumped the rear spar up to reduce the incidence, bumping it > > > up nearly 1/16", then drilled it 5/16". Flew it and found that the > > > left wing felt twice as heavy as the right wing was initially. He then > > > bumped that wing up 1/32" and drilled it 5/16". The next flight it > > > flew hands off and straight. While flying formation I verified > > > sighting down the TE of both wings, all the control surfaces and > > > wingtips are in perfect alignment. > > > > > > I hope to get mine dialed in that well. > > > > > > Regards, > > > Bob Japundza > > > RV-6 flying F1 under const. > > > > > > > > > >


    Message 29


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    Time: 02:01:27 PM PST US
    From: "Ed Anderson" <eanderson@carolina.rr.com>
    Subject: Re: Prop replacement, question for Das Fed, was:
    --> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> Hi Travis, Excellent summary of the requirements on maintenance and inspection for an experimental. However, one thing is not clear - I had my operation limitation amended back about 3 years ago to the effect of giving me the authority to make "Major Modifications" and I simply have to fly a minimum of 5 test hours, record new stall, climb speeds and weight. I entered that data in the log book and a statement to the effect that the aircraft is found safe to fly. There is no indication anywhere that I need to notify the FAA of a "Major Modification" is that not the same as your "Alteration"??. Yes I do have the repairman's certificate for my aircraft. Appreciate you viewpoint to the question Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com ----- Original Message ----- From: "Travis Hamblen" <TravisHamblen@cox.net> <TravisHamblen@cox.net> Subject: Re: RV-List: Prop replacement, question for Das Fed, was: > --> RV-List message posted by: "Travis Hamblen" <TravisHamblen@cox.net> > > Sorry for the late reply... I'm about 10 days behind on the list reading > right now, and this is not meant as a personal stab at anyone, just the > facts. I just wanted to set straight all the misconceptions about > experimental aircraft maintenance. It is shocking to me that people have > such misconceptions about experimental maintenance. First, if you don't > have the repairman certificate for the aircraft in question then you must > have an A&P sign off on the annual conditional inspection (it DOES NOT have > to be an IA). Second, ANYONE can work on an experimental aircraft, major > mods or alterations included. Just make sure you read the operating > limitations, most state that you have to "notify" the FAA of your > alterations before doing them. That means you notify them, not ask > permission. Read the below pasted letter from the EAA about this matter, it > should set the matter straight for any doubters out there. If you still > doubt me, e-mail me and I'll send you a copy of the entire letter and you > can take it to your local FSDO to confirm. This is one of the BEST things > about an experimental; it sidesteps the evil empire (FAA) on most matters. > With all this said, I would warn you not to do anything to an airplane that > you aren't expertly trained in doing, it just may kill you or someone else! > READ ON (not written by me): > > ** "FAR Part 43.1 (b) specifically excludes experimental aircraft so the FAA > is incorrect in stating you are held to any part or appendix of Part 43. It > states "This part does not apply to any aircraft for which an experimental > airworthiness certificate has been issued, unless a different kind of > airworthiness certificate had been previously issued for that aircraft". I > stress the word aircraft so that is not interpreted to include an engine. > What about major repairs and alterations? First you never have to fill > out a form 337 for an experimental aircraft. Repairs major or minor can be > done by anyone, remember Part 43.1 (b). However, alterations are > different. If you alter the aircraft with a different propeller or engine, > for example, then it is not the aircraft for which you received an > airworthiness certificate. This would also apply to changing pistons or > magnetos. It is a new and untested airplane. If you change propellers you > must notify the FAA (not by a 337) of your change. > Your aircraft's operating limitations should have a statement such as > the following in regard to major changes: "The FAA Cognizant Flight > Standards Office must be notified, and their response received in writing, > prior to flying this aircraft after incorporating a major change as defined > by FAR 21.93 > If you do not have such a statement on your operating limitations then > you can claim you do not have to notify the FAA. However, EAA suggest you do > so even if you do not have this limitation. > The FAA inspector will make a determination as to whether he need to > come out and inspect the change and/or assign a new flight-test period. If > the inspector gives you an OK by letter (which is often done) you should > note the date, time, name and change in your aircraft logbook. If the > inspector wants to inspect the aircraft, it is the same as an FAA certified > A&P. So far to EAA's knowledge this has never happened on an amateur built > aircraft. Most operating limitations contain a statement that says and > annual "condition" inspection must be performed per the scope and detail of > FAR Part 43 Appendix D. It also states that an FAA certificated A&P or > repairman must perform this inspection. Note it says "A&P or Repairman". It > does not require an IA. > Let me clarify this. Anyone can work on an experimental aircraft and > sign off the work. However the annual "condition" inspection must be > completed by an A&P or a repairman. > > Sincerely, > Experimental Aircraft Association > Earl Lawrence > Government Programs Specialist" *** > > > Hope that straightens out a bunch of misunderstood maintenance issues, > > Travis > RV-6A @ VGT > RV-7A wiring (in the garage) > > > > gmcjetpilot@yahoo.com wrote: > > > >>--> RV-List message posted by: <gmcjetpilot@yahoo.com> > >> > >> > >>Mike: > >> > >>You are opening a can of worms :- ) The buyer of an experimental aircraft > >>can only do routine maintenance, as if it were a Piper or Cessna, as far > >>as I know. Only the manufacture (builder/repairman) can make major mods, > >>however I assume(?) an A&P or AI could do it and with the FAA's blessing. > >>Again, as in all these matters refer to the FISDO of choice for the > >>answer. There is no "type certificate" configuration for exp a/c, so many > >>changes slip thru the cracks and are not tracked by the FAA. Anyone who > >>has a second hand RV may find them self in a regulatory mess if they want > >>to make a major changes. The best (easiest) thing would get the builder to > > >>sign the mod off if possible. However that is one of the fantastic reasons > > >>for building your own plane. > >> > >>Cheers George > > --- > >


    Message 30


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    Time: 02:12:57 PM PST US
    From: "Sterling" <sterling@pgrb.com>
    Subject: Orndorf videos for sale, $1.00
    --> RV-List message posted by: "Sterling" <sterling@pgrb.com> I just listed on Ebay, at a starting price of $1.00 the Orndorff 2-part empennage videos. If you are interested in a VERY GOOD deal, look up item number 4537703612, or type in "Orndorf Videos" in a search on Ebay. Thanks, Sterling Brooks Knot-2-Shabby Airport & Texas Longhorn Cattle Ranch 5TA6, San Antonio Sectional


    Message 31


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    Time: 02:31:06 PM PST US
    From: Charlie England <ceengland@bellsouth.net>
    Subject: Re: Prop replacement, question for Das Fed, was:
    --> RV-List message posted by: Charlie England <ceengland@bellsouth.net> Ed Anderson wrote: >--> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> > >Hi Travis, > >Excellent summary of the requirements on maintenance and inspection for an >experimental. However, one thing is not clear - I had my operation >limitation amended back about 3 years ago to the effect of giving me the >authority to make "Major Modifications" and I simply have to fly a minimum >of 5 test hours, record new stall, climb speeds and weight. I entered that >data in the log book and a statement to the effect that the aircraft is >found safe to fly. There is no indication anywhere that I need to notify >the FAA of a "Major Modification" is that not the same as your >"Alteration"??. Yes I do have the repairman's certificate for my aircraft. > >Appreciate you viewpoint to the question > >Ed Anderson >RV-6A N494BW Rotary Powered >Matthews, NC >eanderson@carolina.rr.com > snipped Hi Ed, I've done it twice; once pre 911 & once after (different RV-4's). The before was like yours; the after says you have to notify them & get confirmation of test area. Everything changed after 911 & ya gotta protect the public from law abiding citizens now, ya know... I would only trust something in writing from your FSDO but if I had your version I'd use it. Charlie


    Message 32


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    Time: 02:36:57 PM PST US
    From: RVer273sb@aol.com
    Subject: Re: E-mag
    --> RV-List message posted by: RVer273sb@aol.com The folks at E-mag are very devoted to producing a quality product. They want to get the few bugs out of their product so there won't be problems in the field for the customers. I have never delt with more sincere and honest people.The wait for your ordered e-mags will be rewarded with a reliable product. I was one of the first customers and don't regret my decision to purchase their products. They are nice compact units and operation with them is supurb. Stewart, Rv4 in colorado


    Message 33


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    Time: 03:15:00 PM PST US
    From: "Sterling" <sterling@pgrb.com>
    Subject: Another $1.00 Orndorf Video on Ebay
    --> RV-List message posted by: "Sterling" <sterling@pgrb.com> Sorry to flood the list, but I just added the Orndorf SHEET METAL TOOLS video on Ebay and started the auction at $1.00. You can view this and the Mosler Aircraft Engine Video that I produced for Mosler in 1990 by typing in these item numbers in the respective order. Orndorf Sheet Metal Tools is 4537729428 Ordorf Pre-punched empennage video is 4537703612 Mosler Motors (VW based engine) is 4537719007 Thanks, Sterling Brooks Knot-2-Shabby Airport & Texas Longhorn Cattle Ranch 5TA6, San Antonio Sectional


    Message 34


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    Time: 04:17:02 PM PST US
    From: "Ed Anderson" <eanderson@carolina.rr.com>
    Subject: Re: Prop replacement, question for Das Fed, was:
    --> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> ----- Original Message ----- From: "Charlie England" <ceengland@bellsouth.net> Subject: Re: RV-List: Prop replacement, question for Das Fed, was: > --> RV-List message posted by: Charlie England <ceengland@bellsouth.net> > > Ed Anderson wrote: > > >--> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> > > > >Hi Travis, > > > >Excellent summary of the requirements on maintenance and inspection for an > >experimental. However, one thing is not clear - I had my operation > >limitation amended back about 3 years ago to the effect of giving me the > >authority to make "Major Modifications" and I simply have to fly a minimum > >of 5 test hours, record new stall, climb speeds and weight. I entered that > >data in the log book and a statement to the effect that the aircraft is > >found safe to fly. There is no indication anywhere that I need to notify > >the FAA of a "Major Modification" is that not the same as your > >"Alteration"??. Yes I do have the repairman's certificate for my aircraft. > > > >Appreciate you viewpoint to the question > > > >Ed Anderson > >RV-6A N494BW Rotary Powered > >Matthews, NC > >eanderson@carolina.rr.com > > > > snipped > Hi Ed, > I've done it twice; once pre 911 & once after (different RV-4's). The > before was like yours; the after says you have to notify them & get > confirmation of test area. Everything changed after 911 & ya gotta > protect the public from law abiding citizens now, ya know... > > I would only trust something in writing from your FSDO but if I had > your version I'd use it. > > Charlie > Thanks Charlie, I think I'll stay in compliance with the Operating limitations I currently have {:>). When having it done, I offered up a test area to the east of my airpatch which is mainly open farm land and the FSDO simply stated it wasn't necessary as "I knew" no flights of experimentals were permitted over heavily populate areas? Hoping my prop will be back by the end of this week. Ed


    Message 35


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    Time: 04:52:19 PM PST US
    From: Jsd41@aol.com
    Subject: AILERON TRIM SPRINGS
    --> RV-List message posted by: Jsd41@aol.com List: I am installing my aileron trim in my RV-6A. Is there something other then safety wire to attach the springs to the adjusting lever? It seem like it will be hard to get both side adjusted. Thanks Jerry Davis Glen Carbon, ILL


    Message 36


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    Time: 05:30:39 PM PST US
    From: "Ed Anderson" <eanderson@carolina.rr.com>
    Subject: Re: AILERON TRIM SPRINGS
    --> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> I used safety wire and it seems to work well. But, perhaps I just got lucky. Ed Anderson Rv-6A N494BW Rotary Powered Matthew, NC eanderson@carolina.rr.com ----- Original Message ----- From: <Jsd41@aol.com> Subject: RV-List: AILERON TRIM SPRINGS > --> RV-List message posted by: Jsd41@aol.com > > List: > I am installing my aileron trim in my RV-6A. Is there something other then > safety wire to attach the springs to the adjusting lever? It seem like it will > be hard to get both side adjusted. > Thanks > Jerry Davis > Glen Carbon, ILL > >


    Message 37


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    Time: 05:45:51 PM PST US
    From: Hopperdhh@aol.com
    Subject: Re: AILERON TRIM SPRINGS
    --> RV-List message posted by: Hopperdhh@aol.com Jerry, You could just skip that step IMHO. I used .041 safety wire. But, I have found that I never use the trim lever anyway. It is not very easy to get to because my seats have only about 2 inches (if that much) room between them. Also, I have had trouble keeping it adjusted tight enough to hold. I am going to remove the springs and see if I miss having the trim. I use the Nav-Aid autopilot a lot, so it is not necessary to have the airplane trimmed perfectly. When I am flying the airplane, I never notice it being out of trim. It is so light on the controls that almost no stick force will keep it level. I may get flamed, but the plane doesn't fly hands off anyway -- almost but not hands off. Dan Hopper Walton, IN RV-7A (In the paint shop for a long time) --> RV-List message posted by: Jsd41@aol.com List: I am installing my aileron trim in my RV-6A. Is there something other then safety wire to attach the springs to the adjusting lever? It seem like it will be hard to get both side adjusted. Thanks Jerry Davis Glen Carbon, ILL


    Message 38


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    Time: 06:09:28 PM PST US
    From: Jim Oke <wjoke@shaw.ca>
    Subject: Re: AILERON TRIM SPRINGS
    --> RV-List message posted by: Jim Oke <wjoke@shaw.ca> When the time came to install my aileron springs, it just happened that installing the springs directly between the bottom of the trim handle and the tabs at the base of the sticks came out "just right". No need for safety wire or whatever. I tried some combinations of wire but all attempts ended up with the springs too slack. So maybe I just got lucky too. Have a look at http://www.vansairforce.org/projects/okej/onephoto.cgi?Picture_0615.jpg for my installation. Yes, the springs may look over-extended but the control feel when flying is just fine. Jim Oke RV-6A, C-GKGZ Wpg., MB ----- Original Message ----- From: "Ed Anderson" <eanderson@carolina.rr.com> Subject: Re: RV-List: AILERON TRIM SPRINGS > --> RV-List message posted by: "Ed Anderson" <eanderson@carolina.rr.com> > > I used safety wire and it seems to work well. But, perhaps I just got > lucky. > > Ed Anderson > Rv-6A N494BW Rotary Powered > Matthew, NC > eanderson@carolina.rr.com > > ----- Original Message ----- > From: <Jsd41@aol.com> > To: <rv-list@matronics.com> > Subject: RV-List: AILERON TRIM SPRINGS > > >> --> RV-List message posted by: Jsd41@aol.com >> >> List: >> I am installing my aileron trim in my RV-6A. Is there something other > then >> safety wire to attach the springs to the adjusting lever? It seem like it > will >> be hard to get both side adjusted. >> Thanks >> Jerry Davis >> Glen Carbon, ILL >> >> > > >


    Message 39


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    Time: 06:15:56 PM PST US
    From: "Pat Hatch" <pat_hatch@msn.com>
    Subject: AILERON TRIM SPRINGS
    --> RV-List message posted by: "Pat Hatch" <pat_hatch@msn.com> Jerry, I used R/C threaded links and ball links. The ball links get screwed into the actuator arm (one on each side). Then connect the balls to the springs with the quick links. Works really well and the threaded links are adjustable. Available at most hobby shops that deal in R/C stuff. Here is a picture of the same thing on my flap position actuator which will give you the idea. http://home.bellsouth.net/p/s/community.dll?ep=87&subpageid=148112&ck Hope this helps. Pat Hatch RV-6 RV-7 List: I am installing my aileron trim in my RV-6A. Is there something other then safety wire to attach the springs to the adjusting lever? It seem like it will be hard to get both side adjusted. Thanks Jerry Davis


    Message 40


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    Time: 09:46:27 PM PST US
    From: <gmcjetpilot@yahoo.com>
    Subject: Canopy Breaker Survival Gear
    --> RV-List message posted by: <gmcjetpilot@yahoo.com> What is the best tool to carry to chop your way out of an RV on its back? After reading how a pilot and passenger flipped their RV on it's back and needed to hack their way-out by breaking the canopy enough with a fire extinguisher, I started looking for some suitable tools. Here are few suggestions I found, but looking for any comments? "Aircrew Survival Egress Knife" (ASEK) Survival System http://www.rangerjoes.com/product_info.php?products_id=1987 "Bush Pilot Hatchet" (shop around) http://www.cozycamping.net/camping-gear-11427.html?src=froogle-cozycamping OR http://www.policegearusa.com/showitem.cfm/23625/13940.htm Multi-functional tool - Ax, a hatchet, a pry bar and hammer http://www.cheaperthandirt.com/ctd/product.asp?sku=MLT-5105 "Pilot survival knife" with hammer handle http://west.loadup.com/military/surplus/755.html SafeAirs canopy - "Bubble Buster" (bottom of page center) http://www.safeair1.com/index.htm Any suggestions on the best way to break the canopy for emergency egress? Cheers George


    Message 41


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    Time: 11:05:05 PM PST US
    From: Mickey Coggins <mick-matronics@rv8.ch>
    Subject: Re: Prop replacement, question for Das Fed, was:
    --> RV-List message posted by: Mickey Coggins <mick-matronics@rv8.ch> There was a recent article in one of the aviation magazines (flying, kitplanes, aopa pilot - can't recall which) which discussed the case of a guy not being covered in an accident because he made "major" modifications without notifying the FAA. He apparently did a lot of damage on the ground during the accident, and even though the crash had nothing to do with the supposedly "major" modifications, the insurance company was able to weasel out of coverage. Seemed like a very nasty situation. Mickey -- Mickey Coggins http://www.rv8.ch/ #82007 Wiring




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