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References: [ +from:enquiries@europaaviation.co.uk: 154 ]

Total 154 documents matching your query.

21. Re: Tri-gear HELP!! (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 14 Jan 1997 10:13:08
relaxed dimension, and you will need to allow approximately 2" per side on top of this for the deflection of the legs under load. You also need a bit extra if you intend fitting spats. One other poi
/europa_forum//html/europa-list/1997-01/msg00059.html (8,196 bytes)

22. Re: Outrigger Latch Trimming (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 21 Jan 1997 09:33:33
Your clearance of.028" is O.K. The geometry requires an "overcentre" to stop vibration, shock loads, etc. from collapsing the outrigger mechanism. This overcentre does give clearance of the order yo
/europa_forum//html/europa-list/1997-01/msg00098.html (9,430 bytes)

23. Re: Washout errors... (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 3 Feb 1997 09:25:15
there is washout it can't be the possible, then incidence, (& at 70% He's a If you do as Graham suggests, which is a good way of averaging out any deviations from the theoretical washout, then the w
/europa_forum//html/europa-list/1997-02/msg00001.html (8,267 bytes)

24. Re: OR5 (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 11 Feb 1997 13:33:22
unacceptably high friction loads in the mechanism to cause the spring OR12 to extend at all before the outrigger leg has latched down, or that you are maybe operating the mechanism with the wing lead
/europa_forum//html/europa-list/1997-02/msg00064.html (9,320 bytes)

25. Re: Micro Encoders and Static system (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 11 Feb 1997 13:33:25
A quick-connect coupling suitable for the pitot is the PLC-12 Polypropylene coupling from Colder Products Company. Ensure that you order the type with push-on hose connections as opposed to the thre
/europa_forum//html/europa-list/1997-02/msg00065.html (8,056 bytes)

26. Re: Drill Precision (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 11 Feb 1997 13:33:27
The rivets used are metric and the drill sizes are quoted from the manufacturer's data. However the number 30 drill should be close enough. Note that a 4.8mm drill is used to make holes for AN3 bolt
/europa_forum//html/europa-list/1997-02/msg00066.html (9,155 bytes)

27. Re: Windscreen Demist (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 11 Feb 1997 13:33:29
vanes. A simple filter, similar to the inlet filter, should sort out that problem though. Whether the air will be warm enough will have to be found out from experimentation. Regards Andy Draper -- W
/europa_forum//html/europa-list/1997-02/msg00067.html (8,115 bytes)

28. Re: Re: OR5 (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Fri, 14 Feb 1997 11:35:26
Rihard wrote:-...... except to say that if the slot in OR5 >was< a bit I do see your point that if the slot were shorter and you did have a broken spring / mud in the mechanism / bent bolt or whateve
/europa_forum//html/europa-list/1997-02/msg00084.html (8,023 bytes)

29. Re: Bolt Lengths (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 18 Feb 1997 08:41:56
In answer to your concern about the counterbore depth for the AN4-31A bolt, you will need to counterbore to a depth of around 15mm, which I agree is more than "slightly deeper than 5mm". The pivot b
/europa_forum//html/europa-list/1997-02/msg00115.html (9,751 bytes)

30. Re: Re: OR5 (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 19 Feb 1997 14:59:14
We have flight tested the Europa using 30=B0 of flap and found that it will tend to levitate before full aileron control is available, or refuse to land until after aileron control has degraded - th
/europa_forum//html/europa-list/1997-02/msg00127.html (7,914 bytes)

31. Re: Variable flaps (was OR5) (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 24 Feb 1997 08:33:17
-- Web Site at www.europa-aviation.co.uk Fax No 44 1751 431706 --
/europa_forum//html/europa-list/1997-02/msg00188.html (8,712 bytes)

32. Re: Your time over again??? (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 24 Feb 1997 08:33:15
The reason for not attempting to describe in the manual the shape required for the rudder's top leading edge such that it could be done prior to fitting to the fin is that I felt it would cause conf
/europa_forum//html/europa-list/1997-02/msg00189.html (8,919 bytes)

33. Re: Aileron/Flap junction. (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 25 Feb 1997 09:09:44
It sounds to me as if the flap is too far aft. The leading edge of the flap should be approximately 3mm from the vertical face of the flap close-out. Andy -- Web Site at www.europa-aviation.co.uk Fa
/europa_forum//html/europa-list/1997-02/msg00203.html (7,623 bytes)

34. Re: Nav-Aid AP ?? (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 25 Feb 1997 09:09:40
The reason that the manual calls for the setting up for the wing lift pin sockets after the fuselage top has been bonded on is due to problems experienced whilst building the production prototype G-
/europa_forum//html/europa-list/1997-02/msg00204.html (7,994 bytes)

35. Re: Variable flaps (was OR5) (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 25 Feb 1997 09:09:38
G-YURO did have a separate flap control in the early days, but the outriggers were always driven from the flap as they are now. Walter Binder from Germany has modified his outriggers to retract elec
/europa_forum//html/europa-list/1997-02/msg00205.html (8,969 bytes)

36. Re: Nav-Aid AP ?? (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 25 Feb 1997 09:09:42
Regarding Nav-Aid autopilots talk to David Dufton (no 16) or Tom Sinclair (no 50) who have both fitted them. Andy -- Web Site at www.europa-aviation.co.uk Fax No 44 1751 431706 --
/europa_forum//html/europa-list/1997-02/msg00206.html (7,980 bytes)

37. Re: Re: Ambiguities???? (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 26 Feb 1997 08:38:13
Let me try to put your mind at rest concerning the depth of counterbore in the port spar for the AN4-31A bolt to carry the CS15P bearing. I agree that my wording of counterboring "slightly deeper" m
/europa_forum//html/europa-list/1997-02/msg00221.html (9,917 bytes)

38. Re: Internet site for Europa. (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 26 Feb 1997 08:38:21
25 Feb.97 Dear Zoe, Thanks for your e-mail. Our URL is HTTP://www.europa-aviation.co.uk and our e-mail address is enquiries@europa-aviation.co.uk. We also have a customer in New Zealand called Tony
/europa_forum//html/europa-list/1997-02/msg00222.html (8,528 bytes)

39. Re: Fitting the instrument module (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 5 Mar 1997 09:16:30
instrument panel: I am afraid you mustn't interrupt the forward lift pin stiffener. You will to go around it with your cables. Regards Andy -- Web Site at www.europa-aviation.co.uk Fax No 44 1751 431
/europa_forum//html/europa-list/1997-03/msg00006.html (7,872 bytes)

40. Re: Fitting the instrument module (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 10 Mar 1997 09:11:28
A solidly embedded tube through the core material of the forward lift pin stiffener would be O.K. I envisaged, from your request, that you would be removing material from the shear webs of the top h
/europa_forum//html/europa-list/1997-03/msg00041.html (8,471 bytes)

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