Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5.1) with ESMTP id 990046 for rob@logan.com; Wed, 19 Dec 2001 14:11:46 -0500 Received: from imo-m05.mx.aol.com ([64.12.136.8]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Wed, 19 Dec 2001 13:47:29 -0500 Received: from Sky2high@aol.com by imo-m05.mx.aol.com (mail_out_v31_r1.9.) id k.29.1fb9f7b6 (1322) for ; Wed, 19 Dec 2001 13:48:03 -0500 (EST) From: Sky2high@aol.com Message-ID: <29.1fb9f7b6.29523ae2@aol.com> Date: Wed, 19 Dec 2001 13:48:02 EST Subject: Re: Lancair 320 unnatural dragging to the left 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 >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Rob and Per, The prop disc better not be perpendicular to the centerline. If I remember correctly, the engine is canted to the right 1.5 degrees. This can also be noted by assembling your cowling off the airplane, setting the aft side on a level surface and noting the side to side slope of the front of the cowling flange. The variation of the engine from the horizontal should have little or no affect on yaw, but on speed (drag). After using soft engine vibration isolators, my engine sagged as much as 3/4 inch from the top of the cowling in flight (measured the bug splatters on the cowl flange). I have shimmed the lower mounts 1/4 inch to now match the cowling, which was built to specs with the engine mounted. I believe the engine also is to have a slight upward cant. The ball is still the best tool (If calibrated to the aircraft references) to straighten out rigging problems. Hands off level flight with the ball centered after trimming all control surfaces is the real measure. Then use your eyes, a mirror and/or formation flight to identify extraordinary displacements of the control surfaces i.e. rudder and elevator horns displaced far from neutral and ailerons not meeting the wingtip. Remember to record the GC and side to side loading imbalances. I don't know about other planes, but about 50 percent (mine included) of a visual survey of 320s at Oshkoosh have a twist at the top of the vertical stab. The moldings also seem to have the trailing edge of the inboard fuselage flap fairing 1/2 inch different horizontally from side to side. Also, I don't know about the fast builds, but slow build vertical stab rib plans were not even close to the moldings -- It is possible to build a vertical lifting wing if the moldings were relied on. In that light, in my airplane, high power climbs and low power operation require right rudder (AOA is "high") and cruise requires some left rudder to keep the ball centered. Scott Krueger N92EX PS. I have a "heavy" left wing, but this was mainly fixed by adjusting the flap rigging and, since I was in "primer", sanded the micro fitted final fairing. The rest was fixed by carrying a compatible enthusiast in the right seat, unbalancing the fuel load or trimming the aileron. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>