Europa-List Digest Archive

Sun 08/28/11


Total Messages Posted: 30



Today's Message Index:
----------------------
 
     1. 01:53 AM - LAA Rally (Steven Pitt)
     2. 02:16 AM - Re: LAA Rally (David Joyce)
     3. 02:24 AM - Re: 914 Prop Question (GRAHAM SINGLETON)
     4. 02:31 AM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (G-IANI)
     5. 02:44 AM - Re: LAA Rally (PHILLIPS I)
     6. 02:52 AM - Re: LAA Rally (goff)
     7. 03:23 AM - Re: LAA Rally (David Joyce)
     8. 03:23 AM - Re: Fuel Filler Neck (GRAHAM SINGLETON)
     9. 03:25 AM - Re: LAA Rally (rayfitton@virginmedia.com)
    10. 05:01 AM - Outrigger Gap (mau11)
    11. 06:12 AM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (jimpuglise@comcast.net)
    12. 06:47 AM - Re: LAA Rally (Mike Gamble)
    13. 07:36 AM - Re: LAA Rally (Bob Harrison)
    14. 08:07 AM - Re: Outrigger Gap (Kevin Klinefelter)
    15. 08:08 AM - Outriggers lenght (mau11)
    16. 08:51 AM - Re: Re: Outrigger Gap (mau11)
    17. 08:51 AM - Re: 914 Prop Question One more thought (Bud Yerly)
    18. 09:10 AM - Tufnol bearings clearances (Andrew Sarangan)
    19. 09:20 AM - Re: Outriggers lenght (Bud Yerly)
    20. 09:29 AM - Re: Tailwheel angle stop & weighing (Bud Yerly)
    21. 09:37 AM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (Rob Housman)
    22. 09:48 AM - Re: LAA Rally (John Heykoop)
    23. 10:30 AM - 914 Prop Question (Erich Trombley)
    24. 10:55 AM - Re: LAA Rally (Steven Pitt)
    25. 10:59 AM - Re: 914 Prop Question One more thought (David Joyce)
    26. 12:20 PM - Re: LAA Rally (Bob Hitchcock)
    27. 01:28 PM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (Robert Borger)
    28. 01:51 PM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (G-IANI)
    29. 03:47 PM - Re: Tufnol bearings clearances (GRAHAM SINGLETON)
    30. 03:54 PM - Re: Mod 71 - Nose gear leg bungee, replacement with springs (Bud Yerly)
 
 
 


Message 1


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    Time: 01:53:29 AM PST US
    From: "Steven Pitt" <steven.pitt2@ntlworld.com>
    Subject: LAA Rally
    On behalf of the Europa Club we would like to get an idea of how many Europas will attend this weekends LAA Rally (2nd to 4th September). We may be able to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of attendance. Don't forget that Swift/Europa Group and members of the Club committee will be in attendance and will be pleased to see you over the weekend - refreshments should be available. Thanks Steve Pitt Chairman, Europa Club


    Message 2


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    Time: 02:16:33 AM PST US
    From: "David Joyce" <davidjoyce@doctors.org.uk>
    Subject: Re: LAA Rally
    Steve, G-XSDJ on Sunday only (apologies for the committee meeting) David Joyce ----- Original Message ----- From: "Steven Pitt" <steven.pitt2@ntlworld.com> Sent: Sunday, August 28, 2011 9:50 AM Subject: Europa-List: LAA Rally On behalf of the Europa Club we would like to get an idea of how many Europas will attend this weekends LAA Rally (2nd to 4th September). We may be able to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of attendance. Don't forget that Swift/Europa Group and members of the Club committee will be in attendance and will be pleased to see you over the weekend - refreshments should be available. Thanks Steve Pitt Chairman, Europa Club


    Message 3


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    Time: 02:24:08 AM PST US
    From: GRAHAM SINGLETON <grahamsingleton@btinternet.com>
    Subject: Re: 914 Prop Question
    Fred,=0Aapologies, I've done it again! I meant flying left hand seat cargo aircraft as =0Aopposed to carrying passengers.=0AGraham=0A=0A=0A=0A=0A=0A__ ______________________________=0AFrom: Fred Klein <fklein@orcasonline.com> =0ATo: europa-list@matronics.com=0ASent: Sunday, 28 August, 2011 5:00:56=0A Subject: Re: Europa-List: 914 Prop Question=0A=0A=0A=0AOn Aug 27, 2011, at 3:33 PM, GRAHAM SINGLETON wrote:=0A=0AI hear that flying transport is a mor e civilsed way to earn a living.=0A=0AGraham...translation needed for (some of) the Yanks...What indeed is "flying =0Atransport"?=0A=0AWould that be t he art of "transporting"?...Is this related to "trainspotting"?=0A=0AFred =============== =0A


    Message 4


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    Time: 02:31:35 AM PST US
    From: "G-IANI" <g-iani@ntlworld.com>
    Subject: Mod 71 - Nose gear leg bungee, replacement with springs
    Rob I have attached a copy of Mod 71 issue 3 for information. The radius of the upper hook should be 38mm to fit the frame tube ( the lower is 32mm). I am not aware of any batch of springs which have been out of tolerance. If yours are please let Europa know. Ian Rickard G-IANI XS Trigear, 300hours Europa Club Mods Specialist e-mail g-iani@ntlworld.com From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Rob Housman Sent: 27 August 2011 21:24 Subject: Europa-List: Mod 71 - Nose gear leg bungee, replacement with springs I've encountered another one of those "minor" problems I have come to accept as normal with the factory's step child, the Tri-Gear. The diameter of the Landing Gear Frame is 1.55 inch (39.4 mm) and the opening in the spring that must hook onto it is 1.35 inch (34.3 mm). This seems to allow for either of two solutions, neither one particularly elegant. 1) use brute force to deform the hook in the spring, 2) cut off some of the end of the hook. Comments and suggestions from those who have perhaps already dealt with this, or anyone else for that matter, would be greatly appreciated. Best regards, Rob Housman Irvine, California Europa XS Rotax 914 S/N A070 Airframe complete Avionics soon


    Message 5


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    Time: 02:44:01 AM PST US
    Subject: Re: LAA Rally
    From: PHILLIPS I <ivor.phillips@ntlworld.com>
    Hi Steve G-IVER i plan on being there for the three days. Ivor Phillips On 28 August 2011 10:14, David Joyce <davidjoyce@doctors.org.uk> wrote: > davidjoyce@doctors.org.uk> > > Steve, G-XSDJ on Sunday only (apologies for the committee meeting) David > Joyce > ----- Original Message ----- From: "Steven Pitt" < > steven.pitt2@ntlworld.com> > To: <europa-list@matronics.com> > Sent: Sunday, August 28, 2011 9:50 AM > Subject: Europa-List: LAA Rally > > > On behalf of the Europa Club we would like to get an idea of how many > Europas will attend this weekends LAA Rally (2nd to 4th September). We may > be able to arrange a dedicated Europa 'line' for parking. Could you please > let me know if you plan to attend with your name, registration and day(s) of > attendance. > Don't forget that Swift/Europa Group and members of the Club committee will > be in attendance and will be pleased to see you over the weekend - > refreshments should be available. > Thanks > Steve Pitt > Chairman, Europa Club > >


    Message 6


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    Time: 02:52:13 AM PST US
    Subject: Re: LAA Rally
    From: "goff" <goffmoore@aviators.net>
    Steve, Peter Field and I will be arriving at 11:04 on the Friday in G-CHOX. Possibility that I may come back on the Sunday. Goff Goff Moore Read this topic online here: http://forums.matronics.com/viewtopic.php?p=350835#350835


    Message 7


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    Time: 03:23:57 AM PST US
    From: David Joyce <stranfaer@btinternet.com>
    Subject: Re: LAA Rally
    Steven I hope to be there early Friday morn GBXGG Rgds David Joyce Sent from the iPad of David Joyce www.eastmidsspas.com On 28 Aug 2011, at 13:50, "Steven Pitt" <steven.pitt2@ntlworld.com> wrote: > On behalf of the Europa Club we would like to get an idea of how many Euro pas will attend this weekends LAA Rally (2nd to 4th September). We may be ab le to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of atten dance. > Don't forget that Swift/Europa Group and members of the Club committee wil l be in attendance and will be pleased to see you over the weekend - refresh ments should be available. > Thanks > Steve Pitt > Chairman, Europa Club > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= >


    Message 8


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    Time: 03:23:57 AM PST US
    From: GRAHAM SINGLETON <grahamsingleton@btinternet.com>
    Subject: Re: Fuel Filler Neck
    The leakage problem is caused by protruding polyethylene moulding flash lin es, =0Aunless the clips are extremely tight the rubber doesn't conform to t he irregular =0Ashape and you get a slight leak.=0AThe tank and the filler neck, "cobra?" are polyethylene, not fibreglass.=0AGraham=0A=0A=0A=0A=0A=0A ________________________________=0AFrom: Gavin and Anne Lee <gavanne@iconz. co.nz>=0ATo: europa-list@matronics.com=0ASent: Sunday, 28 August, 2011 3:14 :17=0ASubject: RE: Europa-List: Fuel Filler Neck=0A=0A=0AHad the same probl em, you need to seal the connections between the metal and the =0Arubber, b est way to do this is with redux (or what ever they call it nowdays) =0Ami x some up and smear it inside the rubber connecting pieces and then reassem ble =0Aand tighten the hose clamps, haven=99t had a problem since=0A =0AGavin Lee ##355 ZK-EPA=0A =0A =0A =0AFrom:owner-europa-list-ser ver@matronics.com =0A[mailto:owner-europa-list-server@matronics.com] On Beh alf Of =0Ajimpuglise@comcast.net=0ASent: Sunday, 28 August 2011 9:15 a.m. =0ATo: Europa List=0ASubject: Europa-List: Fuel Filler Neck=0A =0AI went ou t to calibrate my Princeton Capacitance meter today and the first step =0Ai s to fill the tank. I Have the metal tube between the filler neck and the tank =0Awith a black rubber coupling on each end, between the metal and the glass filler =0Aneck, and the metal and the glass tank. I found that gas leaked a little on =0Aboth ends of the metal tube. When I used a paper tow el to clean the gas off, it =0Ahad a big, black streak on it from the rubbe r coupling tube. More gas, more =0Ablack. The tube looks like radiator ho se, but I am sure it came with the kit. =0AIf avgas is causing it to break down, am I using the proper material on both =0Aends? If not, what should be used?=0A=0AJim Puglise=0AA283 -- Close to flying =0A =0A =0Ahttp:/ /www.matronics.com/Navigator?Europa-List=0A< - MATRONICS WEB FORUMS Same great content also available via the =0AWeb Forums!=0Ahttp://fo rums.matronics.com=0A< - List Contribution Web Site -=0Ahttp://ww =0A


    Message 9


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    Time: 03:25:23 AM PST US
    Subject: Re: LAA Rally
    From: rayfitton@virginmedia.com
    V2h5IG5vdCBsb29rIGF0IFN0d2VsbCB3ZWJwYWdlICxhbGwgYm9va2VkIGFpcmNyYWZ0IGFyZSBs aXN0ZWQNCg0KU2VlIHlvdSB0aGVyZQ0KDQpSYXkNClNlbnQgZnJvbSBteSBCbGFja0JlcnJ5riB3 aXJlbGVzcyBkZXZpY2UNCg0KLS0tLS1PcmlnaW5hbCBNZXNzYWdlLS0tLS0NCkZyb206ICJTdGV2 ZW4gUGl0dCIgPHN0ZXZlbi5waXR0MkBudGx3b3JsZC5jb20+DQpTZW5kZXI6IG93bmVyLWV1cm9w YS1saXN0LXNlcnZlckBtYXRyb25pY3MuY29tDQpEYXRlOiBTdW4sIDI4IEF1ZyAyMDExIDA5OjUw OjEwIA0KVG86IDxldXJvcGEtbGlzdEBtYXRyb25pY3MuY29tPg0KUmVwbHktVG86IGV1cm9wYS1s aXN0QG1hdHJvbmljcy5jb21TdWJqZWN0OiBFdXJvcGEtTGlzdDogTEFBIFJhbGx5DQoNClRoaXMg aXMgYSBtdWx0aS1wYXJ0IG1lc3NhZ2UgaW4gTUlNRSBmb3JtYXQuDQoNCg=


    Message 10


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    Time: 05:01:35 AM PST US
    From: "mau11" <mau11@free.fr>
    Subject: Outrigger Gap
    X-mailer: Foxmail 6, 15, 201, 26 [cn] SGVsbG8gYWxsLA0KSSByZXBsYWNlIG15IG1haW4gd2hlZWwsIG9sZCB0aXJlIGJ5IEFpciB0cmFj IDgwMHg2LCBub3cgdGhlIGRpYW1ldGVyIG9mIHRoZSB3aGVlbCBpcyBiaWdnZXIgYW5kIGl0IGlz IG5lY2Vzc2FyeSB0byByZXBsYWNlIHRoZSBPUjIgb3V0cmlnZ2VyIGxlZyBiZWNhdXNlIHRoZSBn YXAgYmV0d2VlbiBncm91bmQgYW5kIG91dHJpZ2dlciB3aGVlbHMgaXMgdG9vIGJpZy4NCg0KV2hh dCBpcyB0aGUgbm9ybWFsIGdhcCBiZXR3ZWVuIHRoZSBncm91bmQgYW5kIHRoZSBvdXRyaWdnZXIg d2hlZWw/IEkgZG9uJ3QgcmVhZCB0aGlzIGluZm9ybWF0aW9uIG9uIHRoZSBidWlsZGVyIG1hbnVh bC4NCg0KU2VlIHRoZSBkcmF3aW5nIGluY2x1ZGVkDQoNClRoYW5rcyANCk1pY2hlbCBBVVZSQVkN CkJ1aWxkZXIgTrAxNDUgbW9ub3doZWVsIC0gNDAwIGhvdXJzIGZsaWdodA0K


    Message 11


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    Time: 06:12:19 AM PST US
    From: jimpuglise@comcast.net
    Subject: Re: Mod 71 - Nose gear leg bungee, replacement with springs


    Message 12


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    Time: 06:47:47 AM PST US
    From: "Mike Gamble" <mp.gamble@talktalk.net>
    Subject: LAA Rally
    Steve, I hope to be there Friday am for the day only. Mike G-CFMP


    Message 13


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    Time: 07:36:41 AM PST US
    From: "Bob Harrison" <ptag.dev@tiscali.co.uk>
    Subject: LAA Rally
    Hi! Steve I expect to be there Friday only at 0834 local ! I like my eggs sunny side up and the bacon crispy ! Regards Bob H .....G-PTAG From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of David Joyce Sent: 28 August 2011 11:21 Subject: Re: Europa-List: LAA Rally Steven I hope to be there early Friday morn GBXGG Rgds David Joyce Sent from the iPad of David Joyce www.eastmidsspas.com On 28 Aug 2011, at 13:50, "Steven Pitt" <steven.pitt2@ntlworld.com> wrote: On behalf of the Europa Club we would like to get an idea of how many Europas will attend this weekends LAA Rally (2nd to 4th September). We may be able to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of attendance. Don't forget that Swift/Europa Group and members of the Club committee will be in attendance and will be pleased to see you over the weekend - refreshments should be available. Thanks Steve Pitt Chairman, Europa Club 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D


    Message 14


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    Time: 08:07:56 AM PST US
    Subject: Re: Outrigger Gap
    From: Kevin Klinefelter <klinefelter.kevin@gmail.com>
    Michel, The "normal" gap is mostly a matter of personal preference I think. I had the length of the outriggers set so both outriggers just touch with the aircraft fully loaded. I just replaced my Air trac 700x6 (320 hrs,some checking in the sidewall) with the same new tire and it sits a wee bit higher now. I also replaced the tailwheel. I'm not sure that there is a factory specification for the example drawing you attached? This will change as your rubber shock block gets older, too, as well as tire pressure. Kevin On 8/28/11, mau11 <mau11@free.fr> wrote: > Hello all, > I replace my main wheel, old tire by Air trac 800x6, now the diameter of the > wheel is bigger and it is necessary to replace the OR2 outrigger leg because > the gap between ground and outrigger wheels is too big. > > What is the normal gap between the ground and the outrigger wheel? I don't > read this information on the builder manual. > > See the drawing included > > Thanks > Michel AUVRAY > Builder N145 monowheel - 400 hours flight >


    Message 15


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    Time: 08:08:20 AM PST US
    From: "mau11" <mau11@free.fr>
    Subject: Outriggers lenght
    X-mailer: Foxmail 6, 15, 201, 26 [cn] IA0KSGVsbG8gYWxsLA0KSSByZXBsYWNlIG15IG1haW4gd2hlZWwsIG9sZCB0aXJlIGJ5IEFpciB0 cmFjIDgwMHg2LCBub3cgdGhlIGRpYW1ldGVyIG9mIHRoZSB3aGVlbCBpcyBiaWdnZXIgYW5kIGl0 IGlzIG5lY2Vzc2FyeSB0byByZXBsYWNlIHRoZSBPUjIgb3V0cmlnZ2VyIGxlZyBiZWNhdXNlIHRo ZSBnYXAgYmV0d2VlbiBncm91bmQgYW5kIG91dHJpZ2dlciB3aGVlbHMgaXMgdG9vIGJpZy4NCg0K V2hhdCBpcyB0aGUgbm9ybWFsIGdhcCBiZXR3ZWVuIHRoZSBncm91bmQgYW5kIHRoZSBvdXRyaWdn ZXIgd2hlZWw/IEkgZG9uJ3QgcmVhZCB0aGlzIGluZm9ybWF0aW9uIG9uIHRoZSBidWlsZGVyIG1h bnVhbC4NCg0KU2VlIHRoZSBkcmF3aW5nIGluY2x1ZGVkDQoNClRoYW5rcyANCk1pY2hlbCBBVVZS QVkNCkJ1aWxkZXIgTrAxNDUgbW9ub3doZWVsIC0gNDAwIGhvdXJzIGZsaWdodA0K


    Message 16


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    Time: 08:51:53 AM PST US
    From: "mau11" <mau11@free.fr>
    Subject: Re: Outrigger Gap
    X-mailer: Foxmail 6, 15, 201, 26 [cn] VGhhbmtzIEtldmluLA0KWWVzIGkgaW50ZWdyYXRlIGFsbCBvZiB0aGVzZSBwYXJhbWV0ZXJzLCB3 aGVuIEkgc2VlIG1hbnkgcGljdHVyZXMgb2YgbW9ub3doZWVscywgc29tZSBoYXZlIDQgaW5jaGVz IGdhcCBzb21lIG90aGVycyBvdXRyaWdnZXJzIGxlZ3MgYXJlIGNvbXByZXNzZWQgdG8gdGhlIGdy b3VuZC4NClRoZSBhdmVyYWdlIEkgdGhpbmsgaXMgYmV0d2VlbiAxIHRvIDIgaW5jaGVzIGdhcCBh dCBmdWxseSBsb2FkLg0KDQpHb29kIGV2ZW5pbmcNCk1pY2hlbCBBVVZSQVkNCkJ1aWxkZXIgTrAx NDUNCg=


    Message 17


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    Time: 08:51:53 AM PST US
    From: "Bud Yerly" <budyerly@msn.com>
    Subject: Re: 914 Prop Question One more thought
    Tony, One more thought on matching the 914 with a fixed propeller. All advice given by our learned companions is true. I thought I'd throw a couple of numbers I have seen for your decision process. In accomplishing the initial flight test of the LSA version of the Europa, I flew 12AY with two fixed pitch props attached to my 914 Trigear with Classic Wings and XS Fuselage mods... Keep in mind propeller theory is a bit of a zen art as each airframe, engine, turbo system, fuel injected vs carburated, etc. greatly affect the performance as does the blade width, length, twist taper and flexibility. Many times you are comparing apples and oranges. This prop with this engine works great to one guy and is disgusting to another. The prop twist and taper of one custom fixed pitch prop on a trigear is no problem, and in the event of a ground loop in a mono, a very costly mishap. In selecting a prop, the strength of a prop should never be compromised and its ability to absorb abrasion from rain, grass and dirt must be considered in the choices as well as cost and insurance coverage for a prop strike. As all things in an airplane, compromises must be made.. I have tested 64 inch Sensenich ground adjustable two blade and the Warp Drive 64 inch three blade ground adjustable propellers. Both were adjusted to work by minute pitch adjustments. I tweaked until the whole engine/prop combination could be repeatable, dependable, and acceptable to my standards. These standards are: it can't allow the engine to overheat (ground or air), or over speed, or over boost in any normal operation, give a minimum climb of 700 FPM fully loaded at 75 KIAS at full power, cruise at least 120 KIAS at sea level, and climb at max continuous to 10,000 feet (7500 minimum) in 20 minutes or about 500 FPM average. For testing here at my shop it have found the following: Set the pitch so as to get 5200 RPM static at 40 inches of Manifold Pressure (38 if you have the older 914). This drops your power available from 115 HP to about 100 HP. This is a recommendation by Rotax and prevents over boosting and eventual damage. It also is a good all round start for a pitch setting. For the newer 914 engine, that is about 21 degrees (20.5 for the old 914) prop pitch at the tip of the Warp Drive. Takeoff allows the prop to unload while accelerating to about 5500 RPM while at 38 inches and gets you away from the ground quickly at 75 KIAS. Once airborne and above 1000 MSL in a 75 KIAS Climb, begin pulling the throttle back to 100% (out of turbo), the RPM drops disgustingly to about 5000 at 34 inches MP. This greatly reduces the climb, read as dropping the nose a lot. However if the climb speed is increased to 90 KIAS the RPM comes up to about 5300, the MP pressure stays close to the mid 30s and the rate of climb is tolerable and the transition from the 75 to 90 with throttle retard seem natural. Climb to 7500 MSL is reasonable at approximately 700 fpm with one on board and a bit labored at 500 average loaded. Cruise at 5500 MSL tops at about 122 KTAS at 5000 RPM and 31 inches. Max at 5500 RPM and about 35 inches only goes up to about 127. I am working from memory here on Sunday morning so the numbers are ish. I have found with a basic Airmaster AP 332, climb after takeoff is about 1400 FPM, Climb at max continuous starts at 1000 FPM and drops to 4-500 FPM at 10000 MSL. Climbs above 10,000 with the Airmaster start to drop off using the narrow chord Warp Drive blades. Cruise is up from 120 ish to 135 ish at 7500 MSL. Airmaster has now completed and is selling a reverse or Beta with the AP332 for sea planes. Much was done to keep this mod safe and full proof. So for you guys that must have everything, (sea or ski operations), beta is now available. Use with much care. My experience has shown me that the 914 needs a constant speed prop with automatic adjustment (rather than variable pitch) to be properly used and give the full potential of the engine. The constant speed prop eases cockpit workload in high cockpit task operations (takeoff and land), provide a safety margin to prevent over speed, or over boost possibilities in go around or spirited flight situations, improves cruise speed and fuel mileage, and reduces the thrust for short field operations when coming into a short field fully loaded. That said, based on the repair rates of new low time mono pilots and propeller tip damage I have experienced as an Airmaster dealer, a fixed pitch prop used during the initial flight test and learning phase is not a bad decision. It saves initial cost to the mono guys until they are comfortable with the landing characteristics, techniques, etc. It also gives a spare prop for the eventual tip strike or other maintenance action after upgrading to a constant speed. Use care for the CG shift and engine/gearbox/oil system changes during a prop swap. My further testing of the Airmaster two and three blade has been cut short by LSA testing and damage from Sun n Fun taking forever to fix with the backlog of customers in my shop and the painters (customers come first). My apologies to all, but circumstances have delayed any further fixed pitch testing.... Jabiru engine testing with various propellers has been curtailed also, until we can get the Jabiru 3300 in an airplane that will stay cool enough throughout the performance envelope to allow a full test profile. Regards to All, Bud Yerly Europa Tech Support Custom Flight Creations, Inc. www.customflightcreations.com<http://www.customflightcreations.com/> (813) 653-4989 ----- Original Message ----- From: Tony Renshaw<mailto:tonyrenshaw268@gmail.com> To: europa-list@matronics.com<mailto:europa-list@matronics.com> Sent: Saturday, August 27, 2011 10:50 PM Subject: Re: Europa-List: 914 Prop Question,,,,,,,,Thanks for the responses <tonyrenshaw268@gmail.com<mailto:tonyrenshaw268@gmail.com>> Thanks to all that replied regarding the negatives of a Fixed Pitch prop on a 914. It was more a revision of knowledge than a serious desire, but Bob Catto is a very impressive fellow and it got me thinking. As for better abilities in gliding and stopping re pitch settings and other good advice, I am now the wiser. Reg Tony Renshaw On 28/08/2011, at 7:12 AM, David Joyce wrote: <davidjoyce@doctors.org.uk<mailto:davidjoyce@doctors.org.uk>> > > Tony, One benefit of a VP prop that I don't believe has been mentioned but which reference to ground looping brings to mind is that in fine pitch the slowing down effect of the idling prop is very noticeably greater than in coarse pitch. If you are trying to glide somewhere and the prop pitch change system still works, fine pitch is a great asset whereas to stop in a short distance you definitely want it in fine. On T/Off fine pitch also takes you very quickl;y through the dodgy steering phase if you have a mono. Clearly a fixed pitch prop is going to miss out somewhat on both counts. So I guess you are less likely to lose control on the ground and end up ground looping if you have a VP/CS prop. > Incidentally have you looked at the list of flying planes on the Europa Club website where engines & props are listed for pretty much every flying Europa? > Regards, David Joyce, G-XSDJ > > > > http://www.matronics.com/Navigator?Europa-List<http://www.matronics.com/N avigator?Europa-List> http://www.matronics.com/contribution<http://www.matronics.com/contributi on>


    Message 18


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    Time: 09:10:35 AM PST US
    From: Andrew Sarangan <asarangan@gmail.com>
    Subject: Tufnol bearings clearances
    Looking through the email archives, the alignment of the front and rear tufnol bearings/bushings with the aileron torque tube appears to be a critical step in preventing control stiffness. There are no specific guidelines about this on the manual. I am mostly concerned about thermal expansion since the cockpit can see 70C difference from summer to winter. The torque tube is about 24" long and looks like zinc plated steel. For 70C, the thermal expansion will be about 22 mils. So I am thinking I need to insert 12mil shims on either side of the tufnol bearing before bonding the fork and the bushing, and then removing it after cure. Then there is also the question of tufnol expansion due to moisture. There is a chart on tufnol.com on how much tolerance should be allowed for water absorption. This is for prolonged immersion so it can be considered a worst case scenario. For the 1/2" bearing, this translates to about 0.8mm, or about 32mils. So putting both factors together, I am thinking of inserting 25mil shims on both side of the tufnol, for a total of 50mil play. Does this sound right? All of this could turn out to be a moot point if the flex in the cockpit module is a greater factor. Comments are welcome.


    Message 19


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    Time: 09:20:59 AM PST US
    From: "Bud Yerly" <budyerly@msn.com>
    Subject: Re: Outriggers lenght
    Michel, The manual states between 310-312 mm is the length from metal to metal Page 9M-12, but..... Kevin and others have trimmed theirs based on many factors... No two airplanes are the same empty weight and vary their tires from 7-8 inch so distances vary. I have no comment from the factory but I have seen empty on a new build with 7 inch tire 1/2 inch to 1 inch. I personally set up Joe Like's to full of fuel at 0 inch. Jim Brown's is just clear of touching at full fuel no passengers. Others who are competent glider pilots prefer them short to prevent them from digging in. Others use them as training wheels to prevent rocking and they flex quite a bit. Keep the stick back, Bud Yerly Europa Tech Advisor Custom Flight Creations, Inc. www.customflightcreations.com<http://www.customflightcreations.com/> (813) 653-4989 ----- Original Message ----- From: mau11<mailto:mau11@free.fr> To: europa-list@matronics.com<mailto:europa-list@matronics.com> Sent: Sunday, August 28, 2011 11:05 AM Subject: Europa-List: Outriggers lenght Hello all, I replace my main wheel, old tire by Air trac 800x6, now the diameter of the wheel is bigger and it is necessary to replace the OR2 outrigger leg because the gap between ground and outrigger wheels is too big. What is the normal gap between the ground and the outrigger wheel? I don't read this information on the builder manual. See the drawing included Thanks Michel AUVRAY Builder N=B0145 monowheel - 400 hours flight


    Message 20


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    Time: 09:29:38 AM PST US
    From: "Bud Yerly" <budyerly@msn.com>
    Subject: Re: Tailwheel angle stop & weighing
    Graeme, You are on the ideal weight and cg at 60 inches. Enjoy. I install the pins, but do prefer Graham's mod. The pin will hold up in normal operation, but those who insist on pulling the aircraft backwards without a trolley, tend to snap them. I will check if the mod V block alone is available. It works great, it's simple and rugged. It is not that hard to make from 1/2 inch aluminum and a metal cutting band saw and drill press. Bud Yerly Europa Tech Advisor Custom Flight Creations, Inc. www.customflightcreations.com<http://www.customflightcreations.com/> (813) 653-4989 ----- Original Message ----- From: graeme bird<mailto:graeme@gdbmk.co.uk> To: europa-list@matronics.com<mailto:europa-list@matronics.com> Sent: Saturday, August 27, 2011 4:16 AM Subject: Europa-List: Tailwheel angle stop & weighing <graeme@gdbmk.co.uk<mailto:graeme@gdbmk.co.uk>> I am just at final inspection stage but I am not impressed with the small pin as the limit stop having already snapped it off once while moving it around. I have seen a better way that looks to be part of the rod/rudder (graham singleton) mod. I dont want to redo all the inside rudder, but could I just use the limit bit does anyone know, and is it through Europa? Had the plane weighed, by that nice Roy Sears (inexpensive compared to PlaneWeights) measured 369.5 kg 814.6lb but I dont know if thats normal or what also cofg 1.534m 60.2" -------- Graeme Bird G-UMPY Mono Classic/XS FWFD 912ULS/Warp drive FP Build nearing completion Read this topic online here: http://forums.matronics.com/viewtopic.php?p=350718#350718<http://forums .matronics.com/viewtopic.php?p=350718#350718> http://www.matronics.com/Navigator?Europa-List<http://www.matronics.com/N avigator?Europa-List> http://www.matronics.com/contribution<http://www.matronics.com/contributi on>


    Message 21


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    Time: 09:37:25 AM PST US
    From: "Rob Housman" <rob@hyperion-ef.com>
    Subject: Mod 71 - Nose gear leg bungee, replacement with springs
    Thanks Ian. The plot thickens. I am working from the May 2006 version of the Mod 71 document - THE ONE CURRENTLY AVAILABLE ON THE EUROPA WEB SITE. Just curious since you have already provided it, but other than getting the 2011 version from you, where would I have found it? I hope that this has nothing to do with that little disagreement we had with George III. The dimensions in the latest version match the Landing Gear Frame I have installed although the current LGF is of a significantly different design. And now I know that /U+220538 (Fig. 6, May 2006) means 38 mm. My very slightly larger diameter (39.4 mm) is probably all explained by the powder coat applied by the factory which is apparently no longer done. I'll make things go together per Jeff B's suggestion, implemented in my case with a Dremel and an abrasive cut-off blade. I'll advise the folks in Kirkbymoorside about the opening in my springs. Best regards, Rob Housman Irvine, California Europa XS Rotax 914 S/N A070 Airframe complete Avionics soon From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of G-IANI Sent: Sunday, August 28, 2011 2:29 AM Subject: RE: Europa-List: Mod 71 - Nose gear leg bungee, replacement with springs Rob I have attached a copy of Mod 71 issue 3 for information. The radius of the upper hook should be 38mm to fit the frame tube ( the lower is 32mm). I am not aware of any batch of springs which have been out of tolerance. If yours are please let Europa know. Ian Rickard G-IANI XS Trigear, 300hours Europa Club Mods Specialist e-mail g-iani@ntlworld.com From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Rob Housman Sent: 27 August 2011 21:24 Subject: Europa-List: Mod 71 - Nose gear leg bungee, replacement with springs I've encountered another one of those "minor" problems I have come to accept as normal with the factory's step child, the Tri-Gear. The diameter of the Landing Gear Frame is 1.55 inch (39.4 mm) and the opening in the spring that must hook onto it is 1.35 inch (34.3 mm). This seems to allow for either of two solutions, neither one particularly elegant. 1) use brute force to deform the hook in the spring, 2) cut off some of the end of the hook. Comments and suggestions from those who have perhaps already dealt with this, or anyone else for that matter, would be greatly appreciated. Best regards, Rob Housman Irvine, California Europa XS Rotax 914 S/N A070 Airframe complete Avionics soon


    Message 22


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    Time: 09:48:31 AM PST US
    Subject: Re: LAA Rally
    From: John Heykoop <john.heykoop@gmail.com>
    Hi Steve I am planning to be there Saturday, returning to Goodwood late afternoon. Regards John Heykoop G-JHKP On 28 Aug 2011, at 09:50, "Steven Pitt" <steven.pitt2@ntlworld.com> wrote: > On behalf of the Europa Club we would like to get an idea of how many Euro pas will attend this weekends LAA Rally (2nd to 4th September). We may be ab le to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of atten dance. > Don't forget that Swift/Europa Group and members of the Club committee wil l be in attendance and will be pleased to see you over the weekend - refresh ments should be available. > Thanks > Steve Pitt > Chairman, Europa Club > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= >


    Message 23


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    Time: 10:30:48 AM PST US
    From: "Erich Trombley" <erichdtrombley@juno.com>
    Subject: 914 Prop Question
    Tony, Regarding flying behind a fixed pitch prop and a 914, I did just t hat for a couple of years. As others have mentioned their are a number of benefits to an in-flight adjustable or constant speed prop. Given t hat I live in the desert southwest (Las Vegas, NV) I purchased the 914 f or the express purpose of flying high and I must say I was in fact able to do just that with fixed pitch prop, however, at much slower speeds an d poorer fuel economy than with the NSI prop I currently have. As you climb you will find that one has to continuously throttle back to avoid over-speeding the engine. The higher you go the less power you are able to transfer to the prop and the less efficient it becomes; resulting in a double hit in performance. Installing the NSI was the single biggest performance improvement I have made to the plane, and it is by no means an ideal prop. I would never consider going back to a fixed pitch prop . Just my two cents. Here is a snap shot of a leg from my return trip fr om Oshkosh: 163 KTAS, 124 KIAS , 5 gal/hr fuel flow, 5,000 rpm, 27.7 in MP, 14,300 Pressure Alt, 5 deg C OAT, (16,384 density alt). BTW, this w as the longest leg I have ever flown in the Europa: 5.3 hrs, 745 nautica l miles, 150 KTS ground speed in cruise, 27.3 gallons. If my math is cor rect the above works out to 35 statute miles/gal with a ground speed of 173 M.P.H. Not too shabby for a headwind. My ground speed was even more impressive on the way out OSH. With a tail wind it was over 210 M.P.H at times burning the same 5 gal/hr. I will take that over driving a c ar any day! Kind regards, Erich TrombleyN28ET Classic Mono 914 ____________________________________________________________ Free Quiznos Coupons Celebrate our 30th with Savings. Print Four Great Offers Now! http://thirdpartyoffers.juno.com/TGL3131/4e5a7a8958369937330st04vuc


    Message 24


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    Time: 10:55:04 AM PST US
    From: "Steven Pitt" <steven.pitt2@ntlworld.com>
    Subject: Re: LAA Rally
    Thanks Ray, I did try to find this before sending the email but obviously was not looking in the right place. Steve ----- Original Message ----- From: rayfitton@virginmedia.com To: europa-list@matronics.com Sent: Sunday, August 28, 2011 11:23 AM Subject: Re: Europa-List: LAA Rally Why not look at Stwell webpage ,all booked aircraft are listed See you there Ray ------------------------------------------------------------------------- ----- From: "Steven Pitt" <steven.pitt2@ntlworld.com> Sender: owner-europa-list-server@matronics.com Date: Sun, 28 Aug 2011 09:50:10 +0100 To: <europa-list@matronics.com> ReplyTo: europa-list@matronics.com Subject: Europa-List: LAA Rally On behalf of the Europa Club we would = like to get an idea of how many Europas will attend this weekends LAA Rally (2nd to = 4th September). We may be able to arrange a dedicated Europa 'line' for = parking. Could you please let me know if you plan to attend with your name, = registration and day(s) of attendance. Don't forget that Swift/Europa Group = and members of the Club committee will be in attendance and will be pleased to see you = over the weekend - refreshments should be available. Thanks Steve Pitt Chairman, Europa = Club 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= 3D =B7~=89=B2,=03g'=D3=D3


    Message 25


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    Time: 10:59:31 AM PST US
    From: "David Joyce" <davidjoyce@doctors.org.uk>
    Subject: Re: 914 Prop Question One more thought
    Tony, To compare with the figures Bud has produced so meticulously for fixed pitch props, you may like to compare those I have found with my XS/mono/914 /Woodcomp CS SR 3000 high twist prop and the low twist SR2000 pro at 90 % Max AUW loading: Ground run - Not accurately measured but around 100 metres Climb from1000 to 2000ft: SR3000 40 secs(= 1500fpm) SR2000 42 secs Top True airspeed with100% power at 2000ft SR3000 156 kts SR2000 152 kts at 6500ft SR3000164kts SR2000 160kts The warp drive blade is low twist and I would guess on a CS hub it would give equivalent figures nearer the SR20000 than the SR3000, but even so you will see that climb rate and top speed are dramatically better than with a fixed pitch prop. One other point about the high twist prop is that it produced dramatically better cooling than the SR2000, effectively curing what had always been an issue with my plane ( this is what you would expect theoretically as with low twist blades the inner 1/3 or so of the blade effectively operates in Beta mode at cruise speeds, effectively diverting air from the Europa air inlets!) Regards, David Joyce, G-XSDJ ----- Original Message ----- From: "Bud Yerly" <budyerly@msn.com> Sent: Sunday, August 28, 2011 4:48 PM Subject: Re: Europa-List: 914 Prop Question One more thought Tony, One more thought on matching the 914 with a fixed propeller. All advice given by our learned companions is true. I thought I'd throw a couple of numbers I have seen for your decision process. In accomplishing the initial flight test of the LSA version of the Europa, I flew 12AY with two fixed pitch props attached to my 914 Trigear with Classic Wings and XS Fuselage mods... Keep in mind propeller theory is a bit of a zen art as each airframe, engine, turbo system, fuel injected vs carburated, etc. greatly affect the performance as does the blade width, length, twist taper and flexibility. Many times you are comparing apples and oranges. This prop with this engine works great to one guy and is disgusting to another. The prop twist and taper of one custom fixed pitch prop on a trigear is no problem, and in the event of a ground loop in a mono, a very costly mishap. In selecting a prop, the strength of a prop should never be compromised and its ability to absorb abrasion from rain, grass and dirt must be considered in the choices as well as cost and insurance coverage for a prop strike. As all things in an airplane, compromises must be made.. I have tested 64 inch Sensenich ground adjustable two blade and the Warp Drive 64 inch three blade ground adjustable propellers. Both were adjusted to work by minute pitch adjustments. I tweaked until the whole engine/prop combination could be repeatable, dependable, and acceptable to my standards. These standards are: it can't allow the engine to overheat (ground or air), or over speed, or over boost in any normal operation, give a minimum climb of 700 FPM fully loaded at 75 KIAS at full power, cruise at least 120 KIAS at sea level, and climb at max continuous to 10,000 feet (7500 minimum) in 20 minutes or about 500 FPM average. For testing here at my shop it have found the following: Set the pitch so as to get 5200 RPM static at 40 inches of Manifold Pressure (38 if you have the older 914). This drops your power available from 115 HP to about 100 HP. This is a recommendation by Rotax and prevents over boosting and eventual damage. It also is a good all round start for a pitch setting. For the newer 914 engine, that is about 21 degrees (20.5 for the old 914) prop pitch at the tip of the Warp Drive. Takeoff allows the prop to unload while accelerating to about 5500 RPM while at 38 inches and gets you away from the ground quickly at 75 KIAS. Once airborne and above 1000 MSL in a 75 KIAS Climb, begin pulling the throttle back to 100% (out of turbo), the RPM drops disgustingly to about 5000 at 34 inches MP. This greatly reduces the climb, read as dropping the nose a lot. However if the climb speed is increased to 90 KIAS the RPM comes up to about 5300, the MP pressure stays close to the mid 30s and the rate of climb is tolerable and the transition from the 75 to 90 with throttle retard seem natural. Climb to 7500 MSL is reasonable at approximately 700 fpm with one on board and a bit labored at 500 average loaded. Cruise at 5500 MSL tops at about 122 KTAS at 5000 RPM and 31 inches. Max at 5500 RPM and about 35 inches only goes up to about 127. I am working from memory here on Sunday morning so the numbers are ish. I have found with a basic Airmaster AP 332, climb after takeoff is about 1400 FPM, Climb at max continuous starts at 1000 FPM and drops to 4-500 FPM at 10000 MSL. Climbs above 10,000 with the Airmaster start to drop off using the narrow chord Warp Drive blades. Cruise is up from 120 ish to 135 ish at 7500 MSL. Airmaster has now completed and is selling a reverse or Beta with the AP332 for sea planes. Much was done to keep this mod safe and full proof. So for you guys that must have everything, (sea or ski operations), beta is now available. Use with much care. My experience has shown me that the 914 needs a constant speed prop with automatic adjustment (rather than variable pitch) to be properly used and give the full potential of the engine. The constant speed prop eases cockpit workload in high cockpit task operations (takeoff and land), provide a safety margin to prevent over speed, or over boost possibilities in go around or spirited flight situations, improves cruise speed and fuel mileage, and reduces the thrust for short field operations when coming into a short field fully loaded. That said, based on the repair rates of new low time mono pilots and propeller tip damage I have experienced as an Airmaster dealer, a fixed pitch prop used during the initial flight test and learning phase is not a bad decision. It saves initial cost to the mono guys until they are comfortable with the landing characteristics, techniques, etc. It also gives a spare prop for the eventual tip strike or other maintenance action after upgrading to a constant speed. Use care for the CG shift and engine/gearbox/oil system changes during a prop swap. My further testing of the Airmaster two and three blade has been cut short by LSA testing and damage from Sun n Fun taking forever to fix with the backlog of customers in my shop and the painters (customers come first). My apologies to all, but circumstances have delayed any further fixed pitch testing.... Jabiru engine testing with various propellers has been curtailed also, until we can get the Jabiru 3300 in an airplane that will stay cool enough throughout the performance envelope to allow a full test profile. Regards to All, Bud Yerly Europa Tech Support Custom Flight Creations, Inc. www.customflightcreations.com<http://www.customflightcreations.com/> (813) 653-4989 ----- Original Message ----- From: Tony Renshaw<mailto:tonyrenshaw268@gmail.com> To: europa-list@matronics.com<mailto:europa-list@matronics.com> Sent: Saturday, August 27, 2011 10:50 PM Subject: Re: Europa-List: 914 Prop Question,,,,,,,,Thanks for the responses <tonyrenshaw268@gmail.com<mailto:tonyrenshaw268@gmail.com>> Thanks to all that replied regarding the negatives of a Fixed Pitch prop on a 914. It was more a revision of knowledge than a serious desire, but Bob Catto is a very impressive fellow and it got me thinking. As for better abilities in gliding and stopping re pitch settings and other good advice, I am now the wiser. Reg Tony Renshaw On 28/08/2011, at 7:12 AM, David Joyce wrote: <davidjoyce@doctors.org.uk<mailto:davidjoyce@doctors.org.uk>> > > Tony, One benefit of a VP prop that I don't believe has been mentioned but which reference to ground looping brings to mind is that in fine pitch the slowing down effect of the idling prop is very noticeably greater than in coarse pitch. If you are trying to glide somewhere and the prop pitch change system still works, fine pitch is a great asset whereas to stop in a short distance you definitely want it in fine. On T/Off fine pitch also takes you very quickl;y through the dodgy steering phase if you have a mono. Clearly a fixed pitch prop is going to miss out somewhat on both counts. So I guess you are less likely to lose control on the ground and end up ground looping if you have a VP/CS prop. > Incidentally have you looked at the list of flying planes on the Europa Club website where engines & props are listed for pretty much every flying Europa? > Regards, David Joyce, G-XSDJ > > > > http://www.matronics.com/Navigator?Europa-List<http://www.matronics.com/Navigator?Europa-List> http://www.matronics.com/contribution<http://www.matronics.com/contribution>


    Message 26


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    Time: 12:20:08 PM PST US
    From: "Bob Hitchcock" <robert.hitchcock@virgin.net>
    Subject: Re: LAA Rally
    GBYSA: Sunday only; Bob Hitchcock & Bryan Allsop ----- Original Message ----- From: Steven Pitt To: europa-list@matronics.com Sent: Sunday, August 28, 2011 9:50 AM Subject: Europa-List: LAA Rally On behalf of the Europa Club we would like to get an idea of how many Europas will attend this weekends LAA Rally (2nd to 4th September). We may be able to arrange a dedicated Europa 'line' for parking. Could you please let me know if you plan to attend with your name, registration and day(s) of attendance. Don't forget that Swift/Europa Group and members of the Club committee will be in attendance and will be pleased to see you over the weekend - refreshments should be available. Thanks Steve Pitt Chairman, Europa Club


    Message 27


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    Time: 01:28:59 PM PST US
    From: Robert Borger <rlborger@mac.com>
    Subject: Re: Mod 71 - Nose gear leg bungee, replacement with springs
    Rob, I did Mod 71 at the same time I did the Tri-Gear conversion at Bud's shop. I have pictures of some of the Mod 71 work posted on my Europa Owners site under the conversion album. They are on pages 5 & 6 of the album. We had to grind part of the upper hook point off and round it to obtain a reasonable fit. We also made up a thin stainless steel sheet to go over the Landing Gear Frame under the hooks to help prevent wear to the frame by the hooks (Page 5, about 2/3 of the way down on the right side, IMG_183post). Hope this helps. Blue skies & tailwinds, Bob Borger http://www.europaowners.org/N914XL Europa XS, Short Wing, Intercooled Rotax 914 rlborger@mac.com Cel: 817-992-1117 On Aug 28, 2011, at 11:34 AM, Rob Housman wrote: > Thanks Ian. > > The plot thickens. I am working from the May 2006 version of the Mod 71 document ' THE ONE CURRENTLY AVAILABLE ON THE EUROPA WEB SITE. Just curious since you have already provided it, but other than getting the 2011 version from you, where would I have found it? I hope that this has nothing to do with that little disagreement we had with George III. > > The dimensions in the latest version match the Landing Gear Frame I have installed although the current LGF is of a significantly different design. And now I know that /U+220538 (Fig. 6, May 2006) means 38 mm. My very slightly larger diameter (39.4 mm) is probably all explained by the powder coat applied by the factory which is apparently no longer done. I=92ll make things go together per Jeff B=92s suggestion, implemented in my case with a Dremel and an abrasive cut-off blade. > > I=92ll advise the folks in Kirkbymoorside about the opening in my springs. > > > Best regards, > > Rob Housman > Irvine, California > Europa XS > Rotax 914 > S/N A070 > Airframe complete > Avionics soon


    Message 28


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    Time: 01:51:00 PM PST US
    From: "G-IANI" <g-iani@ntlworld.com>
    Subject: Mod 71 - Nose gear leg bungee, replacement with springs
    Rob At this moment I am the only source of issue 3. At Europa's request (David Goddard said he was too busy) I had it approved by the LAA. I have passed the factory the master copy but as yet they have not got round to putting it up. Mod 77 (Push rod rudder drive) and Mod 78 (Glider wing fix) have gone up recently but the revised versions of 75 and 76 (which include the Dynon servos) are not up yet. The opening for the tube to pass into the spring hook is a bit tight. It is perfectly OK to take off the inside corner to allow the tube in as Jeff B suggested. Ian Rickard G-IANI XS Trigear, 300hours Europa Club Mods Specialist e-mail g-iani@ntlworld.com


    Message 29


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    Time: 03:47:12 PM PST US
    From: GRAHAM SINGLETON <grahamsingleton@btinternet.com>
    Subject: Re: Tufnol bearings clearances
    Andrew=0AYou are right about the problems of thermal expansion etc. I had a problem due =0Ato the clearances being too close. Going from a warm hangar to cold air (flying) =0Athe roll control stiffened up, due to the aluminum contracting quickly and the =0Arest of the airframe slowly. After an hou r the controls had loosened up again.=0AGraham=0A=0A=0A=0A=0A=0A___________ _____________________=0AFrom: Andrew Sarangan <asarangan@gmail.com>=0ATo: E uropa List <europa-list@matronics.com>=0ASent: Sunday, 28 August, 2011 17:0 7:32=0ASubject: Europa-List: Tufnol bearings clearances=0A=0A--> Europa-Lis t message posted by: Andrew Sarangan <asarangan@gmail.com>=0A=0ALooking thr ough the email archives, the alignment of the front and=0Arear tufnol beari ngs/bushings with the aileron torque tube appears to=0Abe a critical step i n preventing control stiffness.=0A=0AThere are no specific guidelines about this on the manual. I am mostly=0Aconcerned about thermal expansion since the cockpit can see 70C=0Adifference from summer to winter. The torque tube is about 24" long=0Aand looks like zinc plated steel. For 70C, the thermal expansion will=0Abe about 22 mils. So I am thinking I need to insert 12mil shims on=0Aeither side of the tufnol bearing before bonding the fork and t he=0Abushing, and then removing it after cure.=0A=0AThen there is also the question of tufnol expansion due to moisture.=0AThere is a chart on tufnol. com on how much tolerance should be allowed=0Afor water absorption. This is for prolonged immersion so it can be=0Aconsidered a worst case scenario. F or the 1/2" bearing, this=0Atranslates to about 0.8mm, or about 32mils.=0A =0ASo putting both factors together, I am thinking of inserting 25mil=0Ashi ms on both side of the tufnol, for a total of 50mil play. Does this=0Asound right?=0A=0AAll of this could turn out to be a moot point if the flex in t =============


    Message 30


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    Time: 03:54:46 PM PST US
    From: "Bud Yerly" <budyerly@msn.com>
    Subject: Re: Mod 71 - Nose gear leg bungee, replacement with springs
    Photo E-mail View slideshow <https://skydrive.live.com/redir.aspx?cid=2161856909618aa7&page=play& resid=2161856909618AA7!136&type=5&authkey=KzlAF!wKhQk%24>| Download images <https://skydrive.live.com/redir.aspx?cid=2161856909618aa7&page=downl oadphotos&resid=2161856909618AA7!136&type=5&authkey=KzlAF!wKhQk%24> Rob, Attached is a drawing of how I round off my springs and a photo of how we keep the spring from grinding into the steel frame by using small bits of stainless. Note that I install the springs with the openning forward. Please note the left and right hand wind requires you to place the springs so that they do not rub against the center tube. The springs can be installed facing aft but the last snap in is a bit difficult unless the entire wheel well is open or you are very strong. Forgive me that I do not have my tech article on how to install the springs any longer as folks were just not having problems and it went to archive somewhere. Bob Borger and Gary Leinberger may have photo's of us doing theirs if you ask.. Please round over the spring as per the drawing to make snapping the spring over the top tube less painful. You may do the lower part as well. One indispensible tool is a piece of stainless cable with handles on both ends to snap the spring up and over the top. I have one of the guys standing on the wheel well and pull it up to snap in the spring over the upper tube. Then he bounces on the front until the 5/16 and 1/4 inch bolts fall out. The other nice to have tool is a set of threaded rods with a couple of curved ends to help hold the gear up while I install, but rope or a strap works also...I just like steel to protect me from a rope brake or strap slip. It takes me with two helpers (for added weight), about 45 minutes to install the springs. <https://skydrive.live.com/redir.aspx?cid=2161856909618aa7&page=play& resid=2161856909618AA7!137&parid=2161856909618AA7!136&type=1&authke y=KzlAF!wKhQk%24> <https://skydrive.live.com/redir.aspx?cid=2161856909618aa7&page=play& resid=2161856909618AA7!138&parid=2161856909618AA7!136&type=1&authke y=KzlAF!wKhQk%24> Small pieces of stainless between the spring and frame glued in or just set in sealant will keep the spring from scratching up your frame and rusting later on. Even with an engine on you can see that putting a cable through the hook on the spring and pulling from above is an easy safe method to snap the spring in. Technique: I normally put the engine on to add weight when I am doing this operation alone. I put a strap around the gearbox and nose gear leg to pull the spring a bit to get the bolts to fall out then repeat. Please use safety precautions so as not to injure yourself when stretching and installing the springs and you will find it is an easy install. Regards, Bud Yerly Europa Tech Advisor Custom Flight Creations, Inc. www.customflightcreations.com<http://www.customflightcreations.com/> (813) 653-4989 ----- Original Message ----- From: G-IANI<mailto:g-iani@ntlworld.com> To: europa-list@matronics.com<mailto:europa-list@matronics.com> Sent: Sunday, August 28, 2011 5:28 AM Subject: RE: Europa-List: Mod 71 - Nose gear leg bungee, replacement with springs Rob I have attached a copy of Mod 71 issue 3 for information. The radius of the upper hook should be 38mm to fit the frame tube ( the lower is 32mm). I am not aware of any batch of springs which have been out of tolerance. If yours are please let Europa know. Ian Rickard G-IANI XS Trigear, 300hours Europa Club Mods Specialist e-mail g-iani@ntlworld.com From: owner-europa-list-server@matronics.com [mailto:owner-europa-list-server@matronics.com] On Behalf Of Rob Housman Sent: 27 August 2011 21:24 To: europa-list@matronics.com Subject: Europa-List: Mod 71 - Nose gear leg bungee, replacement with springs I=92ve encountered another one of those =93minor=94 problems I have come to accept as normal with the factory=92s step child, the Tri-Gear. The diameter of the Landing Gear Frame is 1.55 inch (39.4 mm) and the opening in the spring that must hook onto it is 1.35 inch (34.3 mm). This seems to allow for either of two solutions, neither one particularly elegant. 1) use brute force to deform the hook in the spring, 2) cut off some of the end of the hook. Comments and suggestions from those who have perhaps already dealt with this, or anyone else for that matter, would be greatly appreciated. Best regards, Rob Housman Irvine, California Europa XS Rotax 914 S/N A070 Airframe complete Avionics soon These photos will be available on SkyDrive for 30 days. To learn more about SkyDrive, click here<http://g.msn.com/1cl91enus/PMFooter>. To share high quality pictures with your friends and family using MSN Photo E-mail, join MSN<http://g.msn.com/0PHenus1/29>.




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