Return-Path: Received: from imo18.mx.aol.com ([152.163.225.8]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 25 Dec 1999 11:09:51 -0500 Received: from Sky2high@aol.com by imo18.mx.aol.com (mail_out_v24.6.) id k.0.869a560f (4322) for ; Sat, 25 Dec 1999 11:14:35 -0500 (EST) From: Sky2high@aol.com Message-ID: <0.869a560f.2596476a@aol.com> Date: Sat, 25 Dec 1999 11:14:34 EST Subject: LNC2 Subfloor To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Rob writes: <<< I don't think I've damaged the core, but I sure don't want to be stepping on those areas, particularly if they're covered by carpeting and therefore not visible. So I planned on having my subfloor extend over those areas. >>> You have damaged the core by crushing the nomex. We all have. Stop it. The core, acting as the web, keeps two semi-rigid skins separated at many points. this contributes greatly to the stiffness and strength of the fuselage. If the core is crushed locally, that area is not as rigid. It is locally weaker than before but not as weak as a hole or removal of one of the skins, even if you put back as much glass as in the removed skin. Having said that, the fuselage is very strong and the occasional "weak" spot is probably not going to matter. Nomex cores make the skin very susceptible to puncture damage (your honey's spiked heels or a dropped wrench), but provide the lightest weight for the strength (all moveable control surfaces). For these reasons, the wing skins use foam cores (heavier, more points of support, some give without crushing, stronger structure) and especially the stiffer foam used in the upper stub wing skins so that you can walk on them to get in the plane, spiked heels aside. Build the sub-floor as described in the manual. Why? Because: The 1/4 inch nomex is plenty strong since it is supported and glassed all around. The ramp at the front not only provides extra strength, but is necessary as a foot rest and as a push off point to get out of the plane. The fuselage floor that is exposed is a very small area upon which you will never be able to put any weight because of the instrument panel. In addition, the sub-floor ramp and the main spar provide plenty of strength for that area. The foot rest is important because there are only four (4) positions during cruise flight: a) Both feet forward b) Both feet back (knees up, feet on footrest) c) Left foot forward, right back d) Right foot forward, left back The footrest is needed for three of the four positions. BTW, Use 1/4 inch phenolic hard points and nut plates for the adjustable (fancy) pedals. If you want to remove the pedals or make the cable length adjustable, use turnbuckles on the aft side of the pedals to connect to the rudder cable. Go sit in somebody's LNC2. Scott Krueger N92EX PS: 220 lbs of blubber and I haven't broken my sub-floor or floor yet. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>