Return-Path: Received: from smtp7.gateway.net ([208.230.117.251]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Tue, 21 Mar 2000 13:47:26 -0500 Received: from oemcomputer (1Cust197.tnt1.coeur-dalene.id.da.uu.net [63.27.107.197]) by smtp7.gateway.net (8.9.3/8.9.3) with SMTP id NAA21437 for ; Tue, 21 Mar 2000 13:44:25 -0500 (EST) Message-ID: <000c01bf9366$76ad9d60$c56b1b3f@oemcomputer> Reply-To: "dfs" From: "dfs" To: "Lancair List" Subject: Horiz stab mod Date: Tue, 21 Mar 2000 10:51:25 -0800 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Howdy all. Been off galivanting for the last two weeks or so, so this is a late response to the subject. I like the small horizontal stab. N235SP is an early 235 (hull # 52) with a slightly warmed O-235-L2C on which the original horizontal stab has been just peachy-keen for over 500 hours of flying. This airplane has had it's envelope fully expanded to about 5 - 8 MPH IAS beyond redline at about 100 ft MSL (yes, it was done in very small increments) without even the beginning hint of a problem. It has been flown heavy ;-) at or near the aft CG with no problem. I have never run out of elevator and I cross the numbers at around 85 MPH IAS on landing. Sure, I have a lot of up-trim dialed in at that time but always have had plenty of elevator to flare as my speed decays even further at touch-down. I'm not willing to perform surgery on my Lancair because some Aussie suits felt the original stab didn't meet some arcane rule. Cheers, Dan Schaefer Again, you pays your money and you takes your choice >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>