[NSRCA-discussion] Integral Landing gear

Verne Koester verne at twmi.rr.com
Fri Feb 26 09:26:11 AKST 2010


You can also get direct copy, molded from the original, Bolly clones from
http://www.aeroproduct.net/ .

 

Verne

 

From: nsrca-discussion-bounces at lists.nsrca.org
[mailto:nsrca-discussion-bounces at lists.nsrca.org] On Behalf Of Joe Lachowski
Sent: Friday, February 26, 2010 11:49 AM
To: NSRCA Discussion List
Subject: Re: [NSRCA-discussion] Integral Landing gear

 

Check with Chris Moon at F3aunlimited.com. He has the Graphtech Bolly Clones
as well as Delro and ZNline CF Gear that probably can be used.
 
> From: vanputte at cox.net
> Date: Fri, 26 Feb 2010 08:51:19 -0600
> To: nsrca-discussion at lists.nsrca.org
> Subject: Re: [NSRCA-discussion] Integral Landing gear
> 
> I can't say whether Graph Tech has a direct replacement for the 
> Integral landing gear, but I'd be very surprised if they didn't. I 
> am very impressed with the quality and prices of their "stuff". 
> Their web site is: http://www.graphtechrcshop.com/ Their e-mail 
> address is ohiocarbon at aol.com and the phone number is 832 335 0328. 
> If you call, Brian may answer the phone, but ask to talk to Mike 
> because he's the one who really knows what's going on.
> 
> Ron
> 
> On Feb 25, 2010, at 11:38 PM, John Gayer wrote:
> 
> >
> > The landing gear legs I received with my Integral weigh 6 ounces 
> > and are very rigid as well. I noticed that when Jason listed the 
> > weights of the components on RC Universe that the gear legs were 
> > listed at 3.2 ounces which is a substantial difference.
> > This will be powered by a YS 170. I haven't checked yet but I 
> > intend to add adjusters if necessary to achieve stab incidence of 
> > 0.0 degrees and a wing incidence of +0.5 degrees.
> >
> > I have three questions that I would like to resolve before I get 
> > any further along.
> >
> > 1. Is there a replacement gear that is lighter and in particular 
> > more flexible? Height of the gear should be about 8 inches.
> > 2. Should the downthrust be reduced from the approximately 2 
> > degrees built into the nose ring to about 0.5 degrees down or ?
> > 3. Should the sidethrust be reduced?
> >
> > Would appreciate help from those of you who have already run into 
> > these problems and found solutions that are working for you.
> >
> > Thanks
> >
> >
> > _______________________________________________
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> > http://lists.nsrca.org/mailman/listinfo/nsrca-discussion
> 
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