Question kinda reminds me of the video (test to failure ;-) where the KR 
goes off the runway into a ditch and explodes, pieces into the air 
everywhere....Then the pilot comes walking out of the 
ditch....Amazing!........Think it was before YouTube?

CldLk-Tim

----- Original Message ----- 
From: "K BURNS" <kjbu...@btinternet.com>
To: <kr...@mylist.net>
Sent: Friday, July 23, 2010 8:23 AM
Subject: KR> Any stress test figures out there for KR 2 wings =max all 
upweight capabilities evidenced for authorities? KR 2 s 1050 auw


Guys,

I am about to take on a KR 2 s project and go down the VW aircooled 
conversion
route and would prefer the more powerful option of a redrive or a type 4 
engine,
(As my knowledge of these units would allow me safer opperation).

I am in the UK and drawings and notes exist for the wing plates etc to take 
the
AUW up to 1050LB, but I have heard of difficulties (within the UK) of having
these mods weight limits accepted.

I would therefore like to send out an appeal to gather data on the weight
capacity of this aircraft, preferably any tests done to destruction within a
measured Labratory enviroment on both the standard wing RAF profile and 
later
"upgraded" version, to compare the slight spar dimentional changes, and foam
cored with wing skin preformed versions .

Personal flight time experience and observed G meter evidence ould also be
valuable as supporting evidence.

I am sure that ther will be many partialy finished /damaged airframes out
there that are destined to go as firewood, and would be better served to be 
used
to test to destrction either in a suitably equiped University or aircraft
research facility(either UK,EU or USA).

I would be willing to act as Hub /organiser for shipping to UK,EU (would 
hope to
contribute to a part loaded container..any offers gratefully recieved).


I have shipped from Pheonix AZ before but I am open to sugestions options, 
(Vans
RV builders container share is one example I know of).

I could go down the simpler route and install a Jabiru engine but I think 
the
technical approach could assist a lot of KR 2 owners who are limited to solo
flight currently,and encourage completion of part finished UK KRs.

I ill be influenced by response (or lack of) as I do not have the resource 
to go
this alone,and also would not want to repeat data collection already 
available.

My aim is to make data obtained to be made freely available subject to any
request for expences to be covered by any univesrities that contribute,or
profesional services engaged or in the case of data copywritten /owned by 
third
parties supplied for this study, subtect to release from any liability for 
use
of that data offered .

I have no previous ties or arrangements regarding this idea and welcome any
possitive/productive suggestions or contributions

Regards

Kevin


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