Europa-List Digest Archive

Wed 09/03/08


Total Messages Posted: 27



Today's Message Index:
----------------------
 
     1. 12:43 AM - Autopilot /Trio Avionics - Dynon (Raimo Toivio)
     2. 01:19 AM - Re: Autopilot /Trio Avionics - Dynon (Frans Veldman)
     3. 01:53 AM - Re: Jos Okhuisen (Frans Veldman)
     4. 02:00 AM - Re: Autopilot /Trio Avionics - Dynon (Paul Mitchell)
     5. 04:29 AM - Re: Autopilot /Trio Avionics - Dynon (peter.rees01@tiscali.co.uk)
     6. 04:29 AM - Re: Rough River Camping area? (sldpileit@aol.com)
     7. 04:41 AM - Off topic- The Tale of The Arab Flight Crew (craig bastin)
     8. 05:39 AM - Re: Jos Okhuisen (josok)
     9. 06:01 AM - Re: Jos Okhuisen (William Daniell)
    10. 07:43 AM - Re: Jos Okhuisen (josok)
    11. 08:46 AM - Re: Off topic- The Tale of The Arab Flight Crew (Rob Housman)
    12. 08:46 AM - Re: Jos Okhuisen (Frans Veldman)
    13. 08:46 AM - Re: Jos Okhuisen (Frans Veldman)
    14. 09:28 AM - Rough River / Jeff Burns (JEFF ROBERTS)
    15. 11:28 AM - Re: Jos Okhuisen (Robert C Harrison)
    16. 11:59 AM - Re: Rough River Camping area? (Paul McAllister)
    17. 12:36 PM - Re: Autopilot /Trio Avionics - Dynon (Karel Vranken)
    18. 12:42 PM - fuel filters (Raimo Toivio)
    19. 02:02 PM - Manifold Pressure Gauge (Carl Pattinson)
    20. 02:16 PM - wiring exit from stick - uk practice? (Rowland & Wilma Carson)
    21. 03:06 PM - Re: Manifold Pressure Gauge (Robert C Harrison)
    22. 03:06 PM - Re: Manifold Pressure Gauge (Frans Veldman)
    23. 03:07 PM - Re: Manifold Pressure Gauge (Terry Seaver (terrys))
    24. 03:09 PM - Re: wiring exit from stick - uk practice? (Robert C Harrison)
    25. 03:38 PM - Re: Manifold Pressure Gauge (David Buckley)
    26. 03:42 PM - Re: wiring exit from stick - uk practice? (David Buckley)
    27. 04:04 PM - Re: Jos Okhuisen (Graham Singleton)
 
 
 


Message 1


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    Time: 12:43:03 AM PST US
    From: "Raimo Toivio" <raimo.toivio@rwm.fi>
    Subject: Autopilot /Trio Avionics - Dynon
    All I have decided to install autopilot, probably one axis only. Trio Avionics Ez Pilot looks neat. Also their customer support seems to be fast and pro, so far. On the other hand, I have in my panel Dynon D10A. I know there is a possibility to update it for Dynons autopilot. That would be much cheaper way but somehow I do not like that idea. What about users experiences? Somebody there - do you have any important info? Thanks, Raimo OH-XRT


    Message 2


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    Time: 01:19:37 AM PST US
    From: Frans Veldman <frans@paardnatuurlijk.nl>
    Subject: Re: Autopilot /Trio Avionics - Dynon
    Hi Raimo, > Trio Avionics Ez Pilot looks neat. > Also their customer support seems to be fast and pro, so far. > > What about users experiences? > Somebody there - do you have any important info? I also decided to use a Trio Avionic's EZ Pilot. I've built it in, but I'm not flying yet. Their customer support is great indeed! Installation is pretty straightforward, I linked the servo to the starboard stick, and put the servo itself under the left thigh support. The nice things are that it really communicates very well with the GPS, and has very nice features, not seen in other auto pilots. The complete installation is very lightweight. Frans


    Message 3


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    Time: 01:53:31 AM PST US
    From: Frans Veldman <frans@paardnatuurlijk.nl>
    Subject: Re: Jos Okhuisen
    Did I miss something, or is there indeed a silence about this subject? I'm about to install a Woodcomp propellor, but I'm holding this off until I have some more insight about the reliability of this system. Also, nobody mentioned it yet, but I'm very interested in the cause of the post landing fire. It is a horrible prospect that this can happen, and I want to take all precautions to minimise this risk. One thing I wonder is how the drain valves affect this risk. They protude from under the skin, and once you glide through a tree or over a rough surface, they will probably break off, and the fuel is free to leak away, possibly inside the cabin if the assembly comes loose, or otherwise under the airplane, which is not desirable as well. Also, not having a switch on the main fuel pump (914) and route it not via the main switch, as the manual recommends, introduces the risk that the fuel pump pumps the entire tank contents inside the cabin after a crash. Of course, having a switch on it introduces another risk: an inadvertently switch off... How do others think about this subject? BTW, it is no longer possible for me to answer on the Europa list via the online forum. The mandatory spell-check malfunctions (it mutters something about a debug mode?). Is there a way to bypass this spell check or can someone switch it off? Frans


    Message 4


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    Time: 02:00:18 AM PST US
    From: "Paul Mitchell" <pm@tecnam.co.uk>
    Subject: Re: Autopilot /Trio Avionics - Dynon
    Hi, I have had both the wing leveller and altitude hold installed in a Tecnam Sierra connected to an Avmap 4 GPS. I had the standard altitude hold without auto trim as the Sierra exhibits very little trim change during flight and so did not go for the auto trim which is available if the aircraft has electric trim fitted. The EZ 2 allows pre set climb or decent rates as well and the EZ 3 does that but with the addition of it also levels off at a pre set height. Over the winter I have built another Sierra and have installing the new Trio Pro Pilot which uses the same servos but all incorporated in one head. This is in fact the wing leveller and EZ3 in one case and is cheaper as a package than the two separate units to the same spec. This will be connected to a "Flymap GPS" but the Trio units uses the standard NMEA 0183 signal link that is common to most GPS. Pre made wiring harnesses are available if required. The Trio does what it says on the box and will fly the aircraft better than you can. As for service, it is superb. I stripped a gear in my first one through clumsiness on my part while adjusting the clutch and they sent me a whole new servo by return.. Paul Mitchell ----- Original Message ----- From: "Frans Veldman" <frans@paardnatuurlijk.nl> Sent: Wednesday, September 03, 2008 9:23 AM Subject: Re: Europa-List: Autopilot /Trio Avionics - Dynon > <frans@paardnatuurlijk.nl> > > Hi Raimo, > >> Trio Avionics Ez Pilot looks neat. >> Also their customer support seems to be fast and pro, so far. >> >> What about users experiences? >> Somebody there - do you have any important info? > > I also decided to use a Trio Avionic's EZ Pilot. I've built it in, but > I'm not flying yet. Their customer support is great indeed! Installation > is pretty straightforward, I linked the servo to the starboard stick, > and put the servo itself under the left thigh support. > The nice things are that it really communicates very well with the GPS, > and has very nice features, not seen in other auto pilots. The complete > installation is very lightweight. > > Frans > > -------------------------------------------------------------------------------- Checked by AVG - http://www.avg.com 17:29


    Message 5


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    Time: 04:29:36 AM PST US
    From: "peter.rees01@tiscali.co.uk" <peter.rees01@tiscali.co.uk>
    Subject: Re: Autopilot /Trio Avionics - Dynon
    I can vouch for the quality of the customer service from Trio - we installed the unit but the data string from our GPS wasn't correct - we shipped the GPS and head back to them and they did a 'special' in the firmware so that it could understand our data stream - they shipped it back to us - total cost 0 (or should that be $0). The only thing that let our installation down was the quality of the servo - we had the old style Navaids servo - the build quality was very poor but they have since realised that and replaced it with a servo of their own design. Peter How safe is your email? - http://www.tiscali.co.uk/products/securemail __________________________________________________________


    Message 6


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    Time: 04:29:36 AM PST US
    Subject: Re: Rough River Camping area?
    From: sldpileit@aol.com
    Rough river state park has camping, and if you want you can camp with your airplane Looking forward to seeing all this weekend.? ??????????????????????????????????????????????????????????Scott and Corky,?N108EA?"Miss Madisyn"???????????????????????????????????????????????? -----Original Message----- From: Rich & Sandy Schultz <TheSchultzFamily@comcast.net> Sent: Tue, 2 Sep 2008 11:33 pm Subject: Europa-List: Rough River Camping area? Does anyone have campsite numbers? I am looking at going if the weather works out and need to set up my reservations and wanted to be in the same area if possible. Rich Schultz N262AE


    Message 7


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    Time: 04:41:00 AM PST US
    From: "craig bastin" <craigb@onthenet.com.au>
    Subject: Off topic- The Tale of The Arab Flight Crew
    This was sent to me by a relative, apparently it was blacked out from the news in europe etc due to Muslim sensitivity concerns Subject: The Tale of The Arab Flight Crew How stupid can you get? Well, this Arab flight crew will show you. Photos Show total destruction of a $200 million aircraft, brand new off the assembly line. THE TALE OF THE ARAB FLIGHT CREW Written by To The Point News Friday, 16 May 2008 The brand spanking new Airbus 340-600, the largest passenger airplane ever built, sat in its hangar inToulouse, France without a single hour of airtime. Enter the Arab flight crew of Abu Dhabi Aircraft Technologies (ADAT) to conduct pre-delivery tests on the ground, such as engine runups, prior to delivery to Etihad Airways in Abu Dhabi . The ADAT crew taxied the A340-600 to the run-up area. Then they took all four engines to takeoff power with a virtually empty aircraft. Not having read the run-up manuals, they had no clue just how light an empty A340-600 really is. The takeoff warning horn was blaring away in the cockpit because they had all 4 engines at full power. The aircraft computers thought they were trying to takeoff but it had not been configured properly (flaps/slats, etc.) Then one of the ADAT crew decided to pull the circuit breaker on the Ground Proximity Sensor to silence the alarm. This fools the aircraft into thinking it is in the air. The computers automatically released all the brakes and set the aircraft rocketing forward. The ADAT crew had no idea that this is a safety feature so that pilots can't land with the brakes on. Not one member of the seven-man Arab crew was smart enough to throttle back the engines from their max power setting, so the $200 million brand-new aircraft crashed into a blast barrier, totaling it. The extent of injuries to the crew is unknown, for there has been a news blackout in the major media in France and elsewhere. Coverage of the story was deemed insulting to Moslem Arabs. Finally, the photos are starting to leak out. Airbus $200 million aircraft meets retaining wall and the wall wins....


    Message 8


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    Time: 05:39:26 AM PST US
    Subject: Re: Jos Okhuisen
    From: "josok" <josok-e@ukolo.fi>
    Hi Frans and all, The silence is the normal waiting for the investigation to come to a conclusion. Today i had a long hearing about the course of events. While i have my theory about what happened, i will wait until the final findings are published before commenting. Nethertheless, lets put it this way, my choice will never again be for a propellor without mechanical endstops, in addition to the electrical limit switches. As a minimum i would add run to the outer limits and check outside if the switches are really working and at the right limits. As i found out the hard way, in the air it might be too late. As for the fire risk: Difficult to do better then i did. Possibly, if i would have had one second more time before hitting the trees, i would have followed the emergengy drill better and switched off power before the crash. That maybe would have delayed the fire. Now a thick branch wiped the right side of the cockpit off, breaking the fuel return alu tube. The long range tank (full)survived the blaze i was told. Even with the wheel retracted, the fuel test points stay clear. Hmm, best way to prevent fire is not to crash, but i guess you know that. Regards, Jos Visit - www.EuropaOwners.org


    Message 9


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    Time: 06:01:57 AM PST US
    From: "William Daniell" <wdaniell@etb.net.co>
    Subject: Jos Okhuisen
    Jos I am glad to see you on line again. It is always easy to be wise after the event but each event by its very nature is something new. We have all learned an important lesson from your mishap. Two things strike me: 1. you were remarkably lucky to escape without worse from landing in a tree 2. the fact that it was not worse suggests that the Europa is as safe as it gets. Will -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of josok Sent: Wednesday, September 03, 2008 07:38 Subject: Re: Europa-List: Jos Okhuisen Hi Frans and all, The silence is the normal waiting for the investigation to come to a conclusion. Today i had a long hearing about the course of events. While i have my theory about what happened, i will wait until the final findings are published before commenting. Nethertheless, lets put it this way, my choice will never again be for a propellor without mechanical endstops, in addition to the electrical limit switches. As a minimum i would add run to the outer limits and check outside if the switches are really working and at the right limits. As i found out the hard way, in the air it might be too late. As for the fire risk: Difficult to do better then i did. Possibly, if i would have had one second more time before hitting the trees, i would have followed the emergengy drill better and switched off power before the crash. That maybe would have delayed the fire. Now a thick branch wiped the right side of the cockpit off, breaking the fuel return alu tube. The long range tank (full)survived the blaze i was told. Even with the wheel retracted, the fuel test points stay clear. Hmm, best way to prevent fire is not to crash, but i guess you know that. Regards, Jos Checked by AVG. 17:29


    Message 10


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    Time: 07:43:28 AM PST US
    Subject: Re: Jos Okhuisen
    From: "josok" <josok-e@ukolo.fi>
    Hi Will and all, Before i forget again the most important thing i would like to say: Thank you all for all the snail- email- sms's and phone calls. I knew this is a great community, still all those people living these events with me is more then i did expect. You probably will never know how very important your communications were for me at the worst moments. Yes, in my humble, crah tested opinion, the Europa is a safe plane, not only to fly but also to crash. Still, on more then one account, the accident was not survivable. I was extremely lucky, and the fact that being born Dutch makes me a cheese-head might have helped to maintain consiousness and get out before the fire really started bazing. Regards, Jos Okhuijsrn Visit - www.EuropaOwners.org


    Message 11


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    Time: 08:46:19 AM PST US
    From: "Rob Housman" <rob@hyperion-ef.com>
    Subject: Off topic- The Tale of The Arab Flight Crew
    While the assertion that "Tale of the Arab Flight Crew" has been blacked out because of misplaced sensitivities may be correct, there is reason to suspect the accuracy of the article's main points. The source of this story is "To the Point News" at http://www.tothepointnews.com/content/view/3207/85/ a site that is edited by Dr. Jack Wheeler whose views might be considered a bit outside of the mainstream of contemporary thought. To see why Wheeler might not be playing it straight, see these examples of his political commentary where Wheeler says Obama was using "either amphetamines or cocaine" (http://www.tothepointnews.com/content/view/3208/2/) and McCain is accused of "collaboration with his communist captors" (http://www.worldnetdaily.com/news/article.asp?ARTICLE_ID=60020) Wheeler seems, to me at least, to play it "a bit loose" with the facts. For another on-line report (from a non-political aviation source) of this incident see http://www.flightglobal.com/articles/2007/11/19/219705/toulouse-accident-occ urred-as-airbus-a340-was-exiting-engine-test-pen.html In fairness to Wheeler I must admit that the Flightglobal version lacks substance which in turn lends credence to the Wheeler article. DO NOT ARCHIVE Best regards, Rob Housman Irvine, CA Europa XS Tri-Gear A070 Airframe complete From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of craig bastin Sent: Wednesday, September 03, 2008 4:38 AM Subject: Europa-List: Off topic- The Tale of The Arab Flight Crew This was sent to me by a relative, apparently it was blacked out from the news in europe etc due to Muslim sensitivity concerns Subject: The Tale of The Arab Flight Crew How stupid can you get? Well, this Arab flight crew will show you. Photos Show total destruction of a $200 million aircraft, brand new off the assembly line. THE TALE OF THE ARAB FLIGHT CREW Written by To The Point News Friday, 16 May 2008 The brand spanking new Airbus 340-600, the largest passenger airplane ever built, sat in its hangar inToulouse, France without a single hour of airtime. Enter the Arab flight crew of Abu Dhabi Aircraft Technologies (ADAT) to conduct pre-delivery tests on the ground, such as engine runups, prior to delivery to Etihad Airways in Abu Dhabi . The ADAT crew taxied the A340-600 to the run-up area. Then they took all four engines to takeoff power with a virtually empty aircraft. Not having read the run-up manuals, they had no clue just how light an empty A340-600 really is. The takeoff warning horn was blaring away in the cockpit because they had all 4 engines at full power. The aircraft computers thought they were trying to takeoff but it had not been configured properly (flaps/slats, etc.) Then one of the ADAT crew decided to pull the circuit breaker on the Ground Proximity Sensor to silence the alarm. This fools the aircraft into thinking it is in the air. The computers automatically released all the brakes and set the aircraft rocketing forward. The ADAT crew had no idea that this is a safety feature so that pilots can't land with the brakes on. Not one member of the seven-man Arab crew was smart enough to throttle back the engines from their max power setting, so the $200 million brand-new aircraft crashed into a blast barrier, totaling it. The extent of injuries to the crew is unknown, for there has been a news blackout in the major media in France and elsewhere. Coverage of the story was deemed insulting to Moslem Arabs. Finally, the photos are starting to leak out. Airbus $200 million aircraft meets retaining wall and the wall wins....


    Message 12


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    Time: 08:46:19 AM PST US
    From: Frans Veldman <frans@paardnatuurlijk.nl>
    Subject: Re: Jos Okhuisen
    Hi Jos and all, > Hi Frans and all, The silence is the normal waiting for the > investigation to come to a conclusion. Ok, I understand that. It is just that a few days ago you wrote that you were going to post more detailed information the next day, but I never saw it, so I wondered what happened. Glad that you are still ok. > Now a thick branch wiped the right side of the cockpit off, breaking > the fuel return alu tube. Ok, two toughts about that: 1) The fuel return line is obviously a risk, as it can not be closed with the fuel valve, and once broken it allows the tank to drain completely. I just realised that this risk can be minimised by putting a check-valve (one way valve) in the return line. So fuel can go TO the tank, but never FROM the tank. Has anyone ever considered this? I think I'm going to put this into my fuel system, unless someone can tell me why it is not a good idea to do so. 2) I have seen that many builders do away with the rubber hoses and use aluminium. Maybe the risk is higher with aluminium, since these tubes breaks easily, whereas rubber hoses just give way to impacts. Frans


    Message 13


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    Time: 08:46:19 AM PST US
    From: Frans Veldman <frans@paardnatuurlijk.nl>
    Subject: Re: Jos Okhuisen
    josok wrote: > I was extremely lucky, and the fact > that being born Dutch makes me a cheese-head might have helped to > maintain consiousness and get out before the fire really started > bazing. Well, that you consider being born Dutch made you survive the accident is really encouraging for me. ;-) Frans


    Message 14


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    Time: 09:28:29 AM PST US
    From: JEFF ROBERTS <jeff@rmmm.net>
    Subject: Rough River / Jeff Burns
    HI All, I just got off the cell phone with Jeff Burns of Baby Blue fame. As most of you know he lives in Baton Rough LA and hurricane Gustov's eye came within 20 miles of him. The entire town is without power but he is still planning on driving to Rough River. This can only happen if the power comes back by tomorrow night. They have printing machines with his business he can't leave without power. He ask me to let you all know and he will call me by tomorrow night to let me know one way or the other. I will have his confirmation number should he not come for the cabin as I was planning on splitting it with him. He told me of someone that wanted the couch but I forgot who, so if you get this you can e-mail me direct and know there will be a bedroom open up if he can't make it. I will let everyone know what's going on with him & Mary by tomorrow night. He also said his local EAA hanger was leveled by the storm. Fortunately he's had trouble with Baby Blue and it was in his garage for some repairs. Sometimes it does seem like all things happen for a reason. ;o) Lets keep him in our thoughts. Best Regards, Jeff Roberts A258 - N128LJ / Gold Rush 149 hours and climbing slowly.


    Message 15


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    Time: 11:28:31 AM PST US
    From: "Robert C Harrison" <ptag.dev@tiscali.co.uk>
    Subject: Jos Okhuisen
    Hi! Frans/all As a novice I agree with your suggestion on the "check valve" in the return line and your impact theory for rubber pipes but the latter item would be marginal either way IMHO. The main thing is to apply the maximum delay of fuel spreading to the likely fire source at the front or under you and an element of chance would apply to either type of pipe. This is what has prompted me/many to replace the glass filters under the seat for Andair in the fuselage away from the pilot and /or have a different sight gauge to one encircling the pilot. All such things have to be weight considered otherwise an automatic extinguisher system with heavy tankage to supply but I'm sure you don't need me to remark on that. Regards Bob Harrison G-PTAG -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Frans Veldman Sent: 03 September 2008 16:52 Subject: Re: Europa-List: Jos Okhuisen <frans@paardnatuurlijk.nl> Hi Jos and all, > Hi Frans and all, The silence is the normal waiting for the > investigation to come to a conclusion. Ok, I understand that. It is just that a few days ago you wrote that you were going to post more detailed information the next day, but I never saw it, so I wondered what happened. Glad that you are still ok. > Now a thick branch wiped the right side of the cockpit off, breaking > the fuel return alu tube. Ok, two toughts about that: 1) The fuel return line is obviously a risk, as it can not be closed with the fuel valve, and once broken it allows the tank to drain completely. I just realised that this risk can be minimised by putting a check-valve (one way valve) in the return line. So fuel can go TO the tank, but never FROM the tank. Has anyone ever considered this? I think I'm going to put this into my fuel system, unless someone can tell me why it is not a good idea to do so. 2) I have seen that many builders do away with the rubber hoses and use aluminium. Maybe the risk is higher with aluminium, since these tubes breaks easily, whereas rubber hoses just give way to impacts. Frans


    Message 16


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    Time: 11:59:54 AM PST US
    From: "Paul McAllister" <paul.the.aviator@gmail.com>
    Subject: Re: Rough River Camping area?
    Hi Rich, The Rough River folks let airplane people camp on the grass by there aircraft. The bathrooms at the airstrip have hot showers, and if the weather gets really bad you can just bring your matress & sleeping bag into the FBO office. I have camped many times during the canard fly in event and it has worked out nicely for me. So, in short, there are no assigned campsite number for airplane people and plenty of room and you will be close to everything. Look forward to seeing you there ! Regards, Paul


    Message 17


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    Time: 12:36:56 PM PST US
    From: Karel Vranken <karelvranken@hotmail.com>
    Subject: Autopilot /Trio Avionics - Dynon
    Raimo=2C I have a Trutrak wingleveler and for the 200 hours I have flown it works gr eat. It is slaved to the Garmin 430 and intercepts at the waypoints of the route. Also good after sales service. Best regards=2C Karel Vranken. > From: raimo.toivio@rwm.fi> To: europa-list@matronics.com> Subject: Europa -List: Autopilot /Trio Avionics - Dynon> Date: Wed=2C 3 Sep 2008 10:54:57 + .fi>> > All> > I have decided to install autopilot=2C probably one axis onl y.> > Trio Avionic=B4s Ez Pilot looks neat.> Also their customer support se ems to be fast and pro=2C so far.> > On the other hand=2C I have in my pane l Dynon D10A.> I know there is a possibility to update it for Dynon=B4s aut opilot.> That would be much cheaper way but somehow I do not like that idea .> > What about user=B4s experience=B4s?> Somebody there - do you have any ========================> > >


    Message 18


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    Time: 12:42:33 PM PST US
    From: "Raimo Toivio" <raimo.toivio@rwm-systems.fi>
    Subject: fuel filters
    "This is what has prompted me/many to replace the glass filters > under the seat for Andair in the fuselage away from the pilot" Yes Bob, glass is very bad! I broke one during towing the plane and one went later in the garage by itself. I was full off fuel bathing. Local firearm people adviced me to make thinks beter. Replaced them to the Original Rotax one-piece-plastic ones and have been since happy. Cheap, easy to check and maintain. During possible emergency landing I am sure they (plastic fuel filters) will be my smallest reason for worries. Regards, Raimo OH-XRT ----- Original Message ----- From: "Robert C Harrison" <ptag.dev@tiscali.co.uk> Sent: Wednesday, September 03, 2008 9:26 PM Subject: RE: Europa-List: Jos Okhuisen > <ptag.dev@tiscali.co.uk> > > Hi! Frans/all > As a novice I agree with your suggestion on the "check valve" in the > return line and your impact theory for rubber pipes but the latter item > would be marginal either way IMHO. The main thing is to apply the > maximum delay of fuel spreading to the likely fire source at the front > or under you and an element of chance would apply to either type of > pipe. This is what has prompted me/many to replace the glass filters > under the seat for Andair in the fuselage away from the pilot and /or > have a different sight gauge to one encircling the pilot. > All such things have to be weight considered otherwise an automatic > extinguisher system with heavy tankage to supply but I'm sure you don't > need me to remark on that. > Regards > Bob Harrison G-PTAG > > -----Original Message----- > From: owner-europa-list-server@matronics.com > [mailto:owner-europa-list-server@matronics.com] On Behalf Of Frans > Veldman > Sent: 03 September 2008 16:52 > To: europa-list@matronics.com > Subject: Re: Europa-List: Jos Okhuisen > > <frans@paardnatuurlijk.nl> > > Hi Jos and all, > >> Hi Frans and all, The silence is the normal waiting for the >> investigation to come to a conclusion. > > Ok, I understand that. It is just that a few days ago you wrote that you > were going to post more detailed information the next day, but I never > saw it, so I wondered what happened. Glad that you are still ok. > >> Now a thick branch wiped the right side of the cockpit off, breaking >> the fuel return alu tube. > > Ok, two toughts about that: > > 1) The fuel return line is obviously a risk, as it can not be closed > with the fuel valve, and once broken it allows the tank to drain > completely. I just realised that this risk can be minimised by putting a > check-valve (one way valve) in the return line. So fuel can go TO the > tank, but never FROM the tank. Has anyone ever considered this? I think > I'm going to put this into my fuel system, unless someone can tell me > why it is not a good idea to do so. > > 2) I have seen that many builders do away with the rubber hoses and use > aluminium. Maybe the risk is higher with aluminium, since these tubes > breaks easily, whereas rubber hoses just give way to impacts. > > Frans > > >


    Message 19


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    Time: 02:02:46 PM PST US
    From: "Carl Pattinson" <carl@flyers.freeserve.co.uk>
    Subject: Manifold Pressure Gauge
    X-mailer: iAVMailScanner 1.5.4.5 I am just filling in the LAA form to change our propeller (from a fixed pitch to a CS version - Woodcomp/ Smart Avionics controller). The engine is a Rotax 912 UL 80hp. The LAA form says that the installation of a manifold pressure gauge is mandatory. Anyone know why? Its probably a dumb question but I dont understand the point of monitoring manifold pressure on a normal engine. I always thought it was more relevant to turbocharged engines. Also where does one take the pressure takeoff on the engine - I would guess the balancing pipe between the carburettors - is there a mod required on the engine? Thanks for the explanation in advance. Carl Pattinson G-LABS _______________________________________ No viruses found in this outgoing message Scanned by iolo AntiVirus 1.5.4.5 http://www.iolo.com


    Message 20


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    Time: 02:16:16 PM PST US
    From: Rowland & Wilma Carson <rowil@clara.net>
    Subject: wiring exit from stick - uk practice?
    I'm looking at the bottom of the control stick as I assemble the various parts and am wondering what is the best practice (in UK) for getting the wiring from a switch or switches mounted on the top of the stick out of the stick at or near the bottom. I had a troll through the list archives for various keywords but couldn't find anything relevant, despite having a strong remembrance of the topic being aired not so long ago. I want a PTT at last on the P1 stick, but it would be nice to have a duplicate trim switch there too. (Yes, I'm thinking about shielding them from accidental activation.) Obviously the electrical cable(s) should exit in a place that minimises the chances of (a) fouling up the controls and (b) getting chafed and causing shorts or open circuits. It seems perhaps safest to make a hole in the aft side of the stick (CS16) just above CS01. That way a conventional grommet can easily be fitted, something that might be harder to do if the hole was lower down and passing through the thickness of CS16, CS16B, and CS01. What have other UK builders done that has met with approval from inspectors and (if involved) LAA Engineering? regards Rowland -- | Rowland Carson LAA #16532 http://home.clara.net/rowil/aviation/ | 1100 hours building Europa #435 G-ROWI e-mail <rowil@clara.net>


    Message 21


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    Time: 03:06:24 PM PST US
    From: "Robert C Harrison" <ptag.dev@tiscali.co.uk>
    Subject: Manifold Pressure Gauge
    Hi! Carl Don't know where you take it off on the 912 UL but the 914 has a sensor already plumbed in . You need the manifold pressure to know how much power you are applying ( you could be labouring the engine, since the prop is controlling the RPM the throttle becomes the power applicator. I had this difficulty with the 3300 Jabiru because they wouldn't give me MP/power/RPM/ ambient/altitude graphs I never knew where the engine was loaded until many hours experimenting with fuel usage. Of course the Rotax is geared so the RPM is still more complex. Usually on a direct drive the rule of thumb is to run "squared" = 24" MP to 2,400 Engine Rpm, at least in the initial stages of experimentation. Regards Bob Harrison G-PTAG. -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Carl Pattinson Sent: 03 September 2008 22:01 Subject: Europa-List: Manifold Pressure Gauge <carl@flyers.freeserve.co.uk> I am just filling in the LAA form to change our propeller (from a fixed pitch to a CS version - Woodcomp/ Smart Avionics controller). The engine is a Rotax 912 UL 80hp. The LAA form says that the installation of a manifold pressure gauge is mandatory. Anyone know why? Its probably a dumb question but I dont understand the point of monitoring manifold pressure on a normal engine. I always thought it was more relevant to turbocharged engines. Also where does one take the pressure takeoff on the engine - I would guess the balancing pipe between the carburettors - is there a mod required on the engine? Thanks for the explanation in advance. Carl Pattinson G-LABS _______________________________________ No viruses found in this outgoing message Scanned by iolo AntiVirus 1.5.4.5 http://www.iolo.com


    Message 22


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    Time: 03:06:25 PM PST US
    From: Frans Veldman <frans@paardnatuurlijk.nl>
    Subject: Re: Manifold Pressure Gauge
    Carl Pattinson wrote: > <carl@flyers.freeserve.co.uk> > > I am just filling in the LAA form to change our propeller (from a fixed > pitch to a CS version - Woodcomp/ Smart Avionics controller). The engine > is a Rotax 912 UL 80hp. > > The LAA form says that the installation of a manifold pressure gauge is > mandatory. Anyone know why? A CS prop keeps the rotation speed constant (hence the name Constant Speed prop). The RMP gauge doesn't tell you the engine power anymore, it shows just the prop setting. If you fly with a certain rpm, and throttle back, nothing will change on your rpm gauge as the prop will keep the rpm constant. Hence you won't notice anything as the engine looses power for whatever reason. However, engine power can be determined by looking at the manifold pressure. It is close to ambient pressure if the throttle is wide open, and it will be showing a vacuum at idle, and of course anything in between. Frans


    Message 23


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    Time: 03:07:30 PM PST US
    Subject: Manifold Pressure Gauge
    From: "Terry Seaver (terrys)" <terrys@cisco.com>
    Hi Carl, With a fixed pitch prop, you can get a relative indication of power level from the engine rpm. So on a Cessna 152, your standard procedure might be to pull the power back to 1500 rpm abeam the numbers on down wind. With a constant speed prop, the rpm will be held constant over a wide range of power settings, so the standard measure of power is manifold pressure (although we also use fuel flow often). So on our Europa I would normally pull the power back to 15 inches abeam the numbers. Regards, Terry Seaver -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Carl Pattinson Sent: Wednesday, September 03, 2008 2:01 PM Subject: Europa-List: Manifold Pressure Gauge --> <carl@flyers.freeserve.co.uk> I am just filling in the LAA form to change our propeller (from a fixed pitch to a CS version - Woodcomp/ Smart Avionics controller). The engine is a Rotax 912 UL 80hp. The LAA form says that the installation of a manifold pressure gauge is mandatory. Anyone know why? Its probably a dumb question but I dont understand the point of monitoring manifold pressure on a normal engine. I always thought it was more relevant to turbocharged engines. Also where does one take the pressure takeoff on the engine - I would guess the balancing pipe between the carburettors - is there a mod required on the engine? Thanks for the explanation in advance. Carl Pattinson G-LABS _______________________________________ No viruses found in this outgoing message Scanned by iolo AntiVirus 1.5.4.5 http://www.iolo.com


    Message 24


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    Time: 03:09:44 PM PST US
    From: "Robert C Harrison" <ptag.dev@tiscali.co.uk>
    Subject: wiring exit from stick - uk practice?
    Hi! Rowland Find the place of smallest movement but not to weaken the control stick along with your own appraisals mentioned below. Regards Bob H G-PTAG -----Original Message----- From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Rowland & Wilma Carson Sent: 03 September 2008 17:37 Subject: Europa-List: wiring exit from stick - uk practice? <rowil@clara.net> I'm looking at the bottom of the control stick as I assemble the various parts and am wondering what is the best practice (in UK) for getting the wiring from a switch or switches mounted on the top of the stick out of the stick at or near the bottom. I had a troll through the list archives for various keywords but couldn't find anything relevant, despite having a strong remembrance of the topic being aired not so long ago. I want a PTT at last on the P1 stick, but it would be nice to have a duplicate trim switch there too. (Yes, I'm thinking about shielding them from accidental activation.) Obviously the electrical cable(s) should exit in a place that minimises the chances of (a) fouling up the controls and (b) getting chafed and causing shorts or open circuits. It seems perhaps safest to make a hole in the aft side of the stick (CS16) just above CS01. That way a conventional grommet can easily be fitted, something that might be harder to do if the hole was lower down and passing through the thickness of CS16, CS16B, and CS01. What have other UK builders done that has met with approval from inspectors and (if involved) LAA Engineering? regards Rowland -- | Rowland Carson LAA #16532 http://home.clara.net/rowil/aviation/ | 1100 hours building Europa #435 G-ROWI e-mail <rowil@clara.net>


    Message 25


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    Time: 03:38:16 PM PST US
    From: "David Buckley" <wooburnaviation@googlemail.com>
    Subject: Re: Manifold Pressure Gauge
    If you have a constant speed controller, and there is a loss of power in the engine ( for example from carb ice), the RPM will remain constant ( within the limits of the prop/CS system) as the prop will fine off. The simple way to tell what power the engine is producing, if a power loss occours, is via manifold pressure gauge. On 03/09/2008, Carl Pattinson <carl@flyers.freeserve.co.uk> wrote: > > carl@flyers.freeserve.co.uk> > > I am just filling in the LAA form to change our propeller (from a fixed > pitch to a CS version - Woodcomp/ Smart Avionics controller). The engine is > a Rotax 912 UL 80hp. > > The LAA form says that the installation of a manifold pressure gauge is > mandatory. Anyone know why? > > Its probably a dumb question but I dont understand the point of monitoring > manifold pressure on a normal engine. I always thought it was more relevant > to turbocharged engines. > > Also where does one take the pressure takeoff on the engine - I would guess > the balancing pipe between the carburettors - is there a mod required on the > engine? > > Thanks for the explanation in advance. > > Carl Pattinson > G-LABS > > > _______________________________________ > No viruses found in this outgoing message > Scanned by iolo AntiVirus 1.5.4.5 > http://www.iolo.com > >


    Message 26


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    Time: 03:42:10 PM PST US
    From: "David Buckley" <wooburnaviation@googlemail.com>
    Subject: Re: wiring exit from stick - uk practice?
    I have my only trim switch on the forward face of the stick. I was excellent to use. On 04/09/2008, Robert C Harrison <ptag.dev@tiscali.co.uk> wrote: > > ptag.dev@tiscali.co.uk> > > Hi! Rowland > Find the place of smallest movement but not to weaken the control stick > along with your own appraisals mentioned below. > Regards > Bob H G-PTAG > > -----Original Message----- > From: owner-europa-list-server@matronics.com > [mailto:owner-europa-list-server@matronics.com] On Behalf Of Rowland & > Wilma Carson > Sent: 03 September 2008 17:37 > To: Europa e-mail list > Subject: Europa-List: wiring exit from stick - uk practice? > > <rowil@clara.net> > > I'm looking at the bottom of the control stick as I assemble the > various parts and am wondering what is the best practice (in UK) for > getting the wiring from a switch or switches mounted on the top of > the stick out of the stick at or near the bottom. > > I had a troll through the list archives for various keywords but > couldn't find anything relevant, despite having a strong remembrance > of the topic being aired not so long ago. > > I want a PTT at last on the P1 stick, but it would be nice to have a > duplicate trim switch there too. (Yes, I'm thinking about shielding > them from accidental activation.) > > Obviously the electrical cable(s) should exit in a place that > minimises the chances of (a) fouling up the controls and (b) getting > chafed and causing shorts or open circuits. > > It seems perhaps safest to make a hole in the aft side of the stick > (CS16) just above CS01. That way a conventional grommet can easily be > fitted, something that might be harder to do if the hole was lower > down and passing through the thickness of CS16, CS16B, and CS01. > > What have other UK builders done that has met with approval from > inspectors and (if involved) LAA Engineering? > > regards > > Rowland > -- > >


    Message 27


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    Time: 04:04:41 PM PST US
    From: Graham Singleton <grahamsingleton@btinternet.com>
    Subject: Re: Jos Okhuisen
    Frans & all I agree a check valve might be good. I also think in a serious crash either rubber or aluminum will fail. The most likely cause of fire is electrical, as Jos tells us, first action is to shut off the electrics. In my crash I think the tank split. Battery was at the front and shot off forwards straight away so "automatic switch off" probably occurred as it were. The problem is, when the workload gets too high one forgets the plan, ie "we lose the plot!" I always tell mono drivers to pull stick full back as soon as they feel the tailwheel touch. I never did remember to do it myself, my brain was busy doing something else. Age? maybe but the more you train yourself in these vital actions the more likely you will do it when muck hits fan Graham Robert C Harrison wrote: > > Hi! Frans/all > As a novice I agree with your suggestion on the "check valve" in the > return line > Regards > Bob Harrison G-PTAG




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