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Re: Europa Questions Again

Subject: Re: Europa Questions Again
From: Graham Singleton <grasingleton@avnet.co.uk>
Date: Tue, 25 Jan 2000 00:44:32
 <388A0122.FFE2D527@pali.com>


>Now the Europa Aircraft website lists the limit load
>rating as:
>
>         Europa XS  +3.8G  -1.9G
>
>This would then place it in the "Normal" category and not
>even allow steep turns. Am I missing something?

The problem is the regulations. Because it is a composite airplane load 
factors are more than doubled over that required for a tin and rivets job. 
The Europa wing and center fuselage has demonstrated 8.5 G I understand, 
Andy please correct me.
The reason for the conservative figures is the possibility of a real hot 
day. Composites lose strength quicker than metal at elevated temperatures. 
65 degrees C and above would be hot.
It is also worth noting that extreme cold makes some plastics brittle. 
Gliders have been damaged after cold soak at extreme altitude.

Graham



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