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@matronics.com
[mailto:owner-europa-list-server@matronics.com] Im Auftrag von Fred Klein
Gesendet: Donnerstag, 2. Februar 2012 18:46
An: europa-list@matronics.com
Betreff: Re: AW: Europa-List: Smart engine istalled in a EUROPA
On Feb 2, 2012, at 8:06 AM, uvtreith wrote:
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.
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:
There were and are now cracks and deformations between the firewall/fuselage
and the engine mounting frame.
Did you mean to write that there "are NO cracks and deformations"?...please
explain.
Thanks,
Fred
|