Return-Path: Received: from baron.nii.net ([209.113.172.16]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Wed, 21 Jun 2000 09:08:56 -0400 Received: from nii.net (xcom35.nii.net [209.113.173.99]) by baron.nii.net (8.9.3/8.9.3) with ESMTP id JAA25265 for ; Wed, 21 Jun 2000 09:15:04 -0400 Message-ID: <3950BFA8.4DF79739@nii.net> Date: Wed, 21 Jun 2000 09:14:17 -0400 From: "Angier M. Ames" Reply-To: alphadog@nii.net Organization: Alpha Delta Research To: lancair.list@olsusa.com Subject: Re: Lancair 360FB flaps References: <20000621040630.AAA21464@ns1.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Good morning all, Because the fuselage fillets as they came out of the mold were not quite identical in position, I set the full down flap position relative to a straight edge across the longerons near the rollover. Then, in the full up position of -7 degrees, they were faired in to the fillets. Of course, my concern is that after spending an anal amount of time blending in the flap trailing edge to the fuselage fillet, in flight experience might require an adjustment up or down...thus causing all this "blending time" to be wasted. So, I'm wondering how sensitive are these flaps to small rigging adjustments of perhaps a 1/2 turn on a rod end bearing? Thanks, Angier Ames >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>