Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.7) with ESMTP id 806574 for rob@logan.com; Wed, 04 Jul 2001 21:08:43 -0400 Received: from imo-r01.mx.aol.com ([152.163.225.97]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Wed, 4 Jul 2001 19:09:22 -0400 Received: from RWolf99@aol.com by imo-r01.mx.aol.com (mail_out_v30.22.) id k.8f.cc593f2 (24896) for ; Wed, 4 Jul 2001 19:17:55 -0400 (EDT) From: RWolf99@aol.com Message-ID: <8f.cc593f2.2874fe23@aol.com> Date: Wed, 4 Jul 2001 19:17:55 EDT Subject: Re: Horizontal stabilizer incidence - LNC2 To: lancair.list@olsusa.com MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In a message dated 7/3/2001 11:27:32 PM Pacific Daylight Time, lancair.list@olsusa.com writes: << After a few months of flight on my Lancair 360 (MK II) I have noticed that in level flight the leading edge of the elevator (the counterbalance area) is about 1/4" or 3/8" above the horizontal stabilizer.>> Matt - If your CG is more forward, you would need more down force off the horizontal tail, thus the trailing edge of the tail should be more "up" to generate that extra tail down-force. You have the opposite condition -- you need trailing edge down to get less down-force at the back end of the airplane. Therefore, your suspicion that the forward CG is not the cause is correct. You probably think you have more drag because of the deflected elevator, but then again, you might have less drag overall because the tail generates less downwards lift, you pay for that with less induced drag off the tail, plus your main wing has to generate less lift to compensate for the down force, so there's less induced drag off the main wing as well. But probably you have the same down-force, gotten by having an elevator deflection because the stabilizer is too nose down. Frankly, I don't think you could measure any of those effects on your airspeed indicator. But you could run an experiment where you shift CG to get a different elevator trim position, and see if you notice a change in speed. Is the elevator position a problem, other than the obviously hideous appearance which makes your flying Lancair painful to look at? (Major joke here...) Or do you just want it level for aesthetic reasons? Concerning the stick position, I suspect there is some ability to shorten your forward elevator pushrod to bring the stick aft and closer to vertical. If there's insufficient adjustment, I think you'll have to make a new pushrod, or cut some threads off the existing threaded rod ends. Make sure you can't push a safety wire through the witness holes in the rod end bearing (but you know that). Other than that, I see no problem in adjusting it. You could probably make the aft pushrod a little shorter as well, as long as you leave adequate clearance for the bob-weight. But I'm less certain about this as I haven't gotten that far yet. - Rob Wolf >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>