uvtreith(at)t-online.de Guest
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Posted: Thu Feb 02, 2012 1:29 pm Post subject: AW: AW: Smart engine istalled in a EUROPA |
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Fred,
That is correct. The distributed load was only on 3 engine mounting points instead of 4.
Oh, I missed an no. There were and are NO cracks and deformations ...
Cheers,
Bruno
Von: owner-europa-list-server(at)matronics.com [mailto:owner-europa-list-server(at)matronics.com] Im Auftrag von Fred Klein
Gesendet: Donnerstag, 2. Februar 2012 18:46
An: europa-list(at)matronics.com
Betreff: Re: AW: Smart engine istalled in a EUROPA
On Feb 2, 2012, at 8:06 AM, uvtreith wrote:
Quote: | But one positive thing was: There were and are now cracks and deformations between the firewall/fuselage and the engine mounting frame. The Europa is constructed and built so strong you can trust on.
Nice plane and I am very hot to burn holes in the sky now.
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Bruno,
I salute your perseverence...sorry about that Murphy guy...he's always lurking in the shadows.
If I understand you correctly, the bending of your engine mounting frame during your load test was due to total load being distributed asymmetrically on only 3 of the 4 engine mounting points.
I'm wondering if there is a typo in your sentence above where you write:
Quote: | Quote: | There were and are now cracks and deformations between the firewall/fuselage and the engine mounting frame.
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Did you mean to write that there "are NO cracks and deformations"?...please explain.
Thanks,
Fred
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