Does any one know if the KR wing (original or skins) ever underwent static load
testing. Has Dan ever load tested his wing skins.
Orma
Southfield, MI
N110LR celebrating 20 years
Flying, flying and more flying
http://www.kr-2.aviation-mechanics.com/
List-Post: krnet@list.krnet.org
Date: 12/12/04 12:48:18
To: KRnet
Subject: KR> Static load testing of KR wing
Does any one know if the KR wing (original or skins) ever underwent static
load testing. Has Dan ever load tested his wing skins.
Orma
Southfield, MI
N110LR celebrating 20 years
Flying
I read somewhere that KR wings were tested to destruction
in Australia and they failed at the wing/fuselage transition.
Mac KR2 G-BVZJ - Original Message -
From: "Orma"
To: "KRnet"
Sent: Sunday, December 12, 2004 5:47 PM
Subject: KR> Static load testing of K
and they failed at the wing/fuselage transition
That would make for interesting reading. If you ever find the source
material, I hope you will provide the net with a link.
Orma
Southfield, MI
N110LR celebrating 20 years
Flying, flying and more flying
http://www.kr-2.aviation-mechanics.com/
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