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

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41. Re: Fuel Tank Fittings (score: 1): Author: europa aviation ltd <enquiries@europaaviation.co.uk>; Date: Mon, 10 Mar 1997 09:11:25; Sorry for the late reply, John. The hard copy of your e-mail message got buried in my in tray. What has been missed from fig. 2 in the Mod 33 sheet is that it is a plan view. Therefore the outlets s; /europa_forum//html/europa-list/1997-03/msg00042.html (7,874 bytes)
42. Re: The balancing act (score: 1): Author: europa aviation ltd <enquiries@europaaviation.co.uk>; Date: Tue, 18 Mar 1997 09:07:01; Evidence suggests that the A.P.S. (Aircarft Prepared for Service) c.g. of many Europas is actually well forward. I give below figures of c.g. known to us for flying Europas:- 59.82" AOD 60.28 59.57; /europa_forum//html/europa-list/1997-03/msg00082.html (10,843 bytes)
43. Re: Wing Dimensions (score: 1): Author: europa aviation ltd <enquiries@europaaviation.co.uk>; Date: Wed, 2 Apr 1997 10:09:41; The full chord of the wing is 50" at the root, and 40" at the tip. You can get your other measurements by subtracting your spar to leading edge dimension as made - remembering that one wing is 1.25"; /europa_forum//html/europa-list/1997-04/msg00008.html (7,752 bytes)
44. Re: Weights and c.of. g's (score: 1): Author: europa aviation ltd <enquiries@europaaviation.co.uk>; Date: Wed, 2 Apr 1997 10:09:43; Graham, I purposely did not include weights or identifications of individual aircraft because we did not have owners' permission to publish, and I felt that some owners may not want their weights br; /europa_forum//html/europa-list/1997-04/msg00009.html (7,700 bytes)
45. Re: Mod to Method??? (score: 1): Author: europa aviation ltd <enquiries@europaaviation.co.uk>; Date: Fri, 4 Apr 1997 08:46:21; Blocking the lightening hole slots and allowing the micro to cure is acceptable provided you mask the surrounding foam to prevent micro getting onto it. When you come to do the microing, first mix d; /europa_forum//html/europa-list/1997-04/msg00019.html (8,687 bytes)
46. RE: Jabiru (score: 1): Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>; Date: Thu, 8 May 1997 08:37:53; increase over the other 912 fitted aircraft? Not so much of a performance advantage was found, but we don't experience the performance degradation you would see with the engine breathing the air war; /europa_forum//html/europa-list/1997-05/msg00088.html (9,182 bytes)
47. RE: Gas Tank Grounding ? (score: 1): Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>; Date: Wed, 14 May 1997 09:43:07; We haven't had this problem with a Europa yet, but there is always a first time! Although we have not yet done this, it would be quite straightforward to ground the filler cap to the fuel tank - the; /europa_forum//html/europa-list/1997-05/msg00142.html (9,191 bytes)
48. Re: --- PANIC --- (score: 1): Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>; Date: Thu, 15 May 1997 09:08:11; Without going to the complications of chemical analysis you could carry out a scratch test. If you scratch the surface with a sharp object you should scrape off a white dry swarf. If the epoxy has n; /europa_forum//html/europa-list/1997-05/msg00148.html (8,818 bytes)
49. Re: Door Security (score: 1): Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>; Date: Fri, 16 May 1997 08:52:43; The factory The factory does not recommend filing the tips of the shoot bolts. Are you confusing this with the last para on page 10-27? We're looking closely at the door latch system with a view to p; /europa_forum//html/europa-list/1997-05/msg00159.html (8,297 bytes)
50. Re: Door Security (score: 1): Author: Europa Aviation Ltd <enquiries@europaaviation.co.uk>; Date: Tue, 20 May 1997 10:06:33; I think it's a very valid argument. What does the lazy pilot who can't be bothered to check physically whether the door is closed do when the electric alarm fails to work? It must be added that when; /europa_forum//html/europa-list/1997-05/msg00183.html (8,829 bytes)
51. Re: Damper Mod Nut ? (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Fri, 13 Jun 1997 17:39:40; John, The bolt in question is in shear and not in tension. It is therefore acceptable if necessary to file down the back of the nut to gain the necessary clearance. Regards Roger ____________ Addres; /europa_forum//html/europa-list/1997-06/msg00092.html (7,716 bytes)
52. Re: Mandatory Mod. 40 (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Fri, 13 Jun 1997 17:39:45; Yup! Details in post. Roger ____________ Address for Europa Aviation technical back-up is enquiries@europa-aviation.co.uk; /europa_forum//html/europa-list/1997-06/msg00093.html (7,988 bytes)
53. Re: Mandatory Mod. 40 (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Fri, 20 Jun 1997 08:43:39; Carb ice I'm sure that the debate about carb ice / carb heat on the Rotax 912 will never reach a satisfactory conclusion. I can only reiterate that, with the cold air plenum inlet system fitted to ou; /europa_forum//html/europa-list/1997-06/msg00128.html (8,967 bytes)
54. Re: Mandatory Mod. 40 (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Mon, 23 Jun 1997 09:18:03; Carb ice I'm sure that the debate about carb ice / carb heat on the Rotax 912 will never reach a satisfactory conclusion. I can only reiterate that, with the cold air plenum inlet system fitted to ou; /europa_forum//html/europa-list/1997-06/msg00152.html (8,705 bytes)
55. Re: Plywood (3mm) piece identification (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 08:49:29; Your bits of plywood should be used as follows:- F06 Rear bulkhead Ply-2 Thigh support ribs (3 off) Headrests (2off) Rudder pedal floor (2 off) Ply-3 Spar pin bush reinforcements (these are the ones; /europa_forum//html/europa-list/1997-06/msg00185.html (8,739 bytes)
56. Re: Ailerons (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 08:49:32; centres. bolt. Use overtighten which one The latest issue of the manual does show a dimension from the AN4-10A bolt to the edge of the aileron hinge flange. This dimension is 1.375". The distance to; /europa_forum//html/europa-list/1997-06/msg00186.html (10,076 bytes)
57. Re: Ailerons (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 10:14:20; centres. bolt. Use overtighten which one The latest issue of the manual does show a dimension from the AN4-10A bolt to the edge of the aileron hinge flange. This dimension is 1.375". The distance to; /europa_forum//html/europa-list/1997-06/msg00187.html (10,070 bytes)
58. Re: Plywood (3mm) piece identification (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 10:14:17; Your bits of plywood should be used as follows:- F06 Rear bulkhead Ply-2 Thigh support ribs (3 off) Headrests (2off) Rudder pedal floor (2 off) Ply-3 Spar pin bush reinforcements (these are the ones; /europa_forum//html/europa-list/1997-06/msg00188.html (8,721 bytes)
59. Re: Ailerons (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 11:55:37; centres. bolt. Use overtighten which one The latest issue of the manual does show a dimension from the AN4-10A bolt to the edge of the aileron hinge flange. This dimension is 1.375". The distance to; /europa_forum//html/europa-list/1997-06/msg00189.html (10,075 bytes)
60. Re: Plywood (3mm) piece identification (score: 1): Author: Europa <enquiries@europaaviation.co.uk>; Date: Wed, 25 Jun 1997 11:55:34; Your bits of plywood should be used as follows:- F06 Rear bulkhead Ply-2 Thigh support ribs (3 off) Headrests (2off) Rudder pedal floor (2 off) Ply-3 Spar pin bush reinforcements (these are the ones; /europa_forum//html/europa-list/1997-06/msg00190.html (8,727 bytes)

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