Today's Message Index:
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1. 06:27 AM - Re: 601XL main spar question (sdthatcher)
2. 10:10 AM - Chat Reminder (George Race)
3. 11:57 AM - Re: 601XL main spar question (Ian McClelland)
4. 01:19 PM - Re: 601XL main spar question (Sabrina)
Message 1
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| Subject: | Re: 601XL main spar question |
Sabrina wrote:
> taking a break before my Calc-based Physics E&M test on Monday...
The bird looks great! That wouldn't be Palwaukee airport near Chicago would it?
Will your leading edge cuff be riveted back on or are you going to use camloc or
other connectors?
Let us know what type of movement you get from your testing.
--------
Scott Thatcher, Palm Beach Gardens, FL
601XL with Corvair, Registered as E-LSA
N601EL, EAA203 42 hours and holding.
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=294814#294814
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| Subject: | Re: 601XL main spar question |
I am both curious and alarmed!
What are you doing to your wing? The "D" section provides much strength and
rigidity to the wing structure. Strength will need to be restored before you
fly it again.
Ian McClelland
New Zealand
601xl 90% complete
Upgrade 90% complete
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| Subject: | Re: 601XL main spar question |
Ian,
Are you telling me pink duct tape wont cut it? :O) (That is just to keep the
rain/bird nests out until I have more time )
Dont worry, patch plates will be installed per AC43, as well as L angles riveted
to the D section top and bottom that are connected to the nose rib on each side
On paper, it will be stronger than the original
So far 429 grams added per side
New question, to all:
My NOS AN47 eye bolts just arrived from Preferred Airparts, I have never seen them
with a ring
For those familiar with an AN47 bolt, if you were going to run a 3/16 cable between
two of these AN47 eye bolts, would you cut off the rings or leave them on?
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=294871#294871
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