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

Total 154 documents matching your query.

1. Re: Trim switch ergonomics (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Wed, 2 Oct 1996 12:21:13
We agree that the sense of the trim operation should be as you describe. To state the operation formally:- To trim the aircraft nose up (tab moves down), press the bottom of the rocker switch, and th
/europa_forum//html/europa-list/1996-10/msg00010.html (8,631 bytes)

2. Re: Midwest AE-100 engine information requested (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Fri, 18 Oct 1996 08:31:42
Christoph, The noise level on the Mid West AE-100 is higher than the Rotax, although in fairness we have not yet concentrated on improving the silencer performance. The vibration level is less than
/europa_forum//html/europa-list/1996-10/msg00098.html (8,138 bytes)

3. Re: Decoding Mod Index (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Fri, 25 Oct 1996 13:35:32
Tony A/R means As Required N/A means Not Applicable ff means following pages C/N means Construction Number Page 7 - 10 & ff means Chapter 7 page 10 and following pages. This comes in the Wing Kit se
/europa_forum//html/europa-list/1996-10/msg00134.html (8,760 bytes)

4. Re: Where goes the energy now? (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Tue, 29 Oct 1996 08:34:57
The fact that making the landing gear frame stronger means that the fuselage will see higher stresses has not been ignored here at Europa. The frame will fail before the structure, but not in the ma
/europa_forum//html/europa-list/1996-10/msg00158.html (10,670 bytes)

5. Re: ALL/Amine Blush (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Tue, 29 Oct 1996 08:37:24
As you point out, your discussion with SP Systems indicate that the accuracy they have been recommending to people in the past is not sufficiently strict and should be tightened to 1% of the total mi
/europa_forum//html/europa-list/1996-10/msg00159.html (14,732 bytes)

6. Re: Gear Mods/Ivans Letter (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Tue, 29 Oct 1996 08:33:26
There have been two cases of landing gear frames breaking and one of a partial failure. There are three further reports of frames with cracks in them. In one other case, cracks were reported but hav
/europa_forum//html/europa-list/1996-10/msg00160.html (8,766 bytes)

7. Re: Energy / Landing Gear Frame (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Tue, 29 Oct 1996 08:31:30
It is not required that a CAA licensed welder carry out the welding to your landing gear frame. Use a welder with TIG experience, and who is approved by an engineering company with ISO 5750 or 9000
/europa_forum//html/europa-list/1996-10/msg00161.html (9,196 bytes)

8. Re: Plexi-glass screens - advice please (score: 1)
Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>
Date: Wed, 13 Nov 1996 08:11:54
great) and The Europa was originally to have 2 mm thick Plexiglas screens, but after the moulds had been made it was decided to go for the thicker 3 mm material instead. The method of disguising the
/europa_forum//html/europa-list/1996-11/msg00058.html (8,235 bytes)

9. Build manual index (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 25 Nov 1996 08:19:47
A few weeks ago Barry Wrenford and others rightly lamented the lack of an index in the build manual for the Europa. I have now found time to compile one, which is basically an index of appropriate su
/europa_forum//html/europa-list/1996-11/msg00126.html (7,331 bytes)

10. Mod 37 (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 26 Nov 1996 09:03:47
Reading the various postings on the internet regarding the main gear frame, there seems to be quite a bit of confusion as to the whys and wherefores. It would seem timely to clarify the situation. Ap
/europa_forum//html/europa-list/1996-11/msg00129.html (11,218 bytes)

11. Re: U/C frame (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 26 Nov 1996 09:15:19
The Tri-gear itself does not need Mod 37, but if a monowheel Europa is going to be converted to a Tri-gear, and if it is going to be flown as a monowheel before the conversion, then it will need Mod
/europa_forum//html/europa-list/1996-11/msg00130.html (7,355 bytes)

12. Re: Punctures (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 3 Dec 1996 11:21:39
My feeling is the fault will be with the strength of the tire - Pitts As far as we know the punctures experienced have not been attributed to the brake caliper causing damage. However, the caliper i
/europa_forum//html/europa-list/1996-12/msg00019.html (8,563 bytes)

13. Damper kit / rubber blocks (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Tue, 3 Dec 1996 16:44:37
Recent messages on the Internet suggest an element of confusion about damper kits and rubber blocks. I hope the following explanation may help:- The first damper kits (19 of them in total) were sent
/europa_forum//html/europa-list/1996-12/msg00020.html (9,310 bytes)

14. Re: Damper kit / rubber blocks (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 11 Dec 1996 08:17:46
I Dear Duncan, We have spent a considerable time investigating high hysteresis rubbers for the shock absorber. The conclusion we have come to is that the higher the hysteresis, the greater the creep
/europa_forum//html/europa-list/1996-12/msg00076.html (10,335 bytes)

15. Re: Damper kit / rubber blocks (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 16 Dec 1996 08:52:01
Here's the problem (all figures approximate):- 1 Europa = 1300 lb x 2g landing = 2600 lb (our nominal design case for the shock absorber system - NOT the undercarriage mounting frame strength). Mecha
/europa_forum//html/europa-list/1996-12/msg00100.html (10,189 bytes)

16. Re: Damper kit / rubber blocks (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 16 Dec 1996 08:52:04
Your E-mail message to us has been sent to all and sundry as opposed to our 1/4" packing -- The original shock absorber required a pre-compression to bring the dimension betrween the centres of the
/europa_forum//html/europa-list/1996-12/msg00101.html (12,308 bytes)

17. Christmas holiday arrangements (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Thu, 19 Dec 1996 08:17:36
We shall be closing down for the Christmas and New Year holiday from lunchtime Friday 20th December, reopening on Thursday, 2nd Jan 1997; so if you run short of rivets, bolts, stiffnuts, etc. during
/europa_forum//html/europa-list/1996-12/msg00127.html (7,116 bytes)

18. Re: Home Page (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Mon, 6 Jan 1997 10:15:32
3 January 1997 Dear Jeff Thank you for your enquiry. Not sure whether we can help you regarding the instrument panel, however, you are very welcome to look at our web site. The address is HTTP://www
/europa_forum//html/europa-list/1997-01/msg00020.html (7,363 bytes)

19. Re: Tony's Builder Hints Contest (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 8 Jan 1997 08:05:41
wing easily. Quite right Graham. As the manual does cover a method for making the access hole (in the aileron chapter), and as there's not enough time in the day to start revamping it, I don't envis
/europa_forum//html/europa-list/1997-01/msg00026.html (8,147 bytes)

20. Re: Peel Ply etc. Questions (score: 1)
Author: europa aviation ltd <enquiries@europaaviation.co.uk>
Date: Wed, 8 Jan 1997 08:05:39
Hope the following will help:- A1. A second ply laid onto the previous ply should always be shorter than the first to avoid having a kink and, therefore, weak point. The peel ply on the first fin la
/europa_forum//html/europa-list/1997-01/msg00027.html (9,433 bytes)

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