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21. Re: taildragger conversion (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Mon, 30 Dec 1996 11:21:14; Has anyone taken a look at the implications of of fitting conventional landing gear to the Europa? for: -variable flap settings -tamer runway behaviour -more space (see above) or an extra fuel tank -; /europa_forum//html/europa-list/1996-12/msg00173.html (7,214 bytes)
22. Re: WARNING - Zinc Chromate Primers (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Fri, 3 Jan 1997 22:33:17; Alodyne, Alumiprep (the pre-alodyne acid cleaner -essential) and zinc chromate paint in various forms (spray cans, epoxy 2-packs) are available --From aircraft spruce. The standard aircraft finishing; /europa_forum//html/europa-list/1997-01/msg00011.html (8,490 bytes)
23. Re: Tips (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Wed, 15 Jan 1997 10:20:31; Just a silly one: At last, I have found a use for all those old telephone directories: They are perfect for chopping up and using as infinitely variable spacers for alignment, leveling workbenches an; /europa_forum//html/europa-list/1997-01/msg00064.html (7,367 bytes)
24. BRS update (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 16 Jan 1997 10:56:37; Thanks for the letters of support/encouragement.... After quite a lot of to-ing and fro-ing, we seem to have come up with a workable installation scheme... at least, I think so. It will add about 45; /europa_forum//html/europa-list/1997-01/msg00069.html (7,670 bytes)
25. Washout errors... (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 16 Jan 1997 10:56:35; Having got to the stage of fitting the wing trailing edge blocks to the spar, it has become apparent that there is a small unwanted error in the washout of the wing leading edges; Quite how it got th; /europa_forum//html/europa-list/1997-01/msg00070.html (7,845 bytes)
26. Re: The rudder cable system (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 16 Jan 1997 10:56:34; Has anyone looked at routing the rudder cables through bowden outers whilst in the tunnel? this would allow the cables to be routed hither and thither to clear various things. Venhill engineering (01; /europa_forum//html/europa-list/1997-01/msg00071.html (7,410 bytes)
27. Re: taildragger gear (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 30 Jan 1997 10:45:58; I'm sorry that no-one really rose to the bait of discussing a conventional taildragger Europa.... however, I have been informed that a Swiss and French builder have combined to do exactly that: detai; /europa_forum//html/europa-list/1997-01/msg00121.html (7,247 bytes)
28. Re: Wing Tip Skids (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 30 Jan 1997 10:45:55; stock..... Actually doing them at the moment: 2 mm Titanium stock fabricated 8" X 2", 2 holes drilled and countersunk at the 1/3rd and 2/3rd stations, and a curve rolled onto them (requires quite so; /europa_forum//html/europa-list/1997-01/msg00122.html (8,338 bytes)
29. Re: Windscreen Demist (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sun, 9 Feb 1997 09:55:28; The problem with this is very fine dust blown onto the inside surface of your windscreen: the pump vanes are made from graffite, I believe: not sure I'd want that in my cockpit. Why not duct warm ai; /europa_forum//html/europa-list/1997-02/msg00040.html (7,630 bytes)
30. Re: Micro Encoders and Static system (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Tue, 11 Feb 1997 16:24:25; We are using a co-axial twin tube fitting from Tom Parker Ltd: 01772251405 fx 827088. sealed by "O" rings, positive locking, one half is a bulkhead fitting, made --From plastic for medical equipment; /europa_forum//html/europa-list/1997-02/msg00071.html (7,573 bytes)
31. Flap and aileron cores (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sat, 15 Feb 1997 10:21:18; Perhaps those before me can help out.... (especially those with recent experience -ie wing kits around the #250+ mark) I've been setting out the flap and aileron jig blocks, ready to lay up the parts; /europa_forum//html/europa-list/1997-02/msg00092.html (7,778 bytes)
32. Re: Variable flaps (was OR5) (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sat, 15 Feb 1997 10:46:25; Please tell us more! I have fiddled around with a sketch pad and photocopies of the outrigger mechanism trying to figure out how to have say 2 flap settings, and have the outriggers latch and releas; /europa_forum//html/europa-list/1997-02/msg00093.html (8,392 bytes)
33. Re: Variable flaps (was OR5) (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Tue, 25 Feb 1997 23:15:03; a big Tell us more.... I've been fiddling around with a sketch pad in the evenings for ages, and still haven't come up with a suitable scheme. "American Beer,"<> That being said, as an "overseas memb; /europa_forum//html/europa-list/1997-02/msg00214.html (9,126 bytes)
34. Re: Oversize S3 Foam Blocks (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Mon, 10 Mar 1997 00:53:15; The The foam blocks are something of a variable quantity: 1/4 inch seems to be somewhat excessive -you might want to ask for another one. On my wing, some the blocks had to be packed in places and o; /europa_forum//html/europa-list/1997-03/msg00039.html (9,545 bytes)
35. Re: Capacitance Gauges (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Tue, 18 Mar 1997 09:17:39; There are a couple of things that you should be aware of using capacitance fuel indicators: only some can be bent to compensate for variations in tank volume, so if you intend to do that, order the r; /europa_forum//html/europa-list/1997-03/msg00083.html (8,373 bytes)
36. RE: The balancing act (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Thu, 20 Mar 1997 10:00:34; Perhaps those who send attachments can note what format they are in so we can play with them.... Miles; /europa_forum//html/europa-list/1997-03/msg00098.html (7,946 bytes)
37. Re: BRS project (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sat, 29 Mar 1997 08:03:21; Having failed to come up with any solid reasons NOT to fit a BRS to the FLYER Europa, we are going for it: the unit has been ordered. There has been some speculation as to why we want to fit a BRS to; /europa_forum//html/europa-list/1997-03/msg00128.html (8,220 bytes)
38. Re: Aileron Cores (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sat, 29 Mar 1997 08:03:17; We all suffer from this;There are residual stresses in the foam (from manufacturng) which is released as they are cut up/hot wired. In practice, if you bond the leading edge cores on accurately (in r; /europa_forum//html/europa-list/1997-03/msg00129.html (7,727 bytes)
39. Re: Re: BRS project (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Sun, 30 Mar 1997 20:48:49; They've abandoned this line of defence -in fact, having seen a copy of the CAA's BRS requirement, it boils down to a placard that you must fit that says "Pull the red handle, and the CAA isn't respo; /europa_forum//html/europa-list/1997-03/msg00136.html (7,212 bytes)
40. Re: Parking brake (and dual throttles) (score: 1): Author: Miles McCallum <milesm@avnet.co.uk>; Date: Mon, 31 Mar 1997 17:49:02; My plan on the parking brake is to fit a high quality tap and a one way valve in parallel: the tap will be placed in such a way that it intrudes into the pilots leg when on (probably under the right; /europa_forum//html/europa-list/1997-03/msg00139.html (7,257 bytes)

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