Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.215]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with SMTP id AAA25706 for ; Mon, 21 Sep 1998 10:14:42 -0400 Message-Id: <3.0.3.32.19980921101325.0072f0b8@olsusa.com> Date: Mon, 21 Sep 1998 10:13:25 -0400 To: lancair.list@olsusa.com From: Marvin Kaye Subject: 360 thrust line X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Thanks to Bill Harrelson's loan of his O-320 installation drawings I've managed to locate the thrust line relative to the cups on the dynafocal mount which was supplied by the factory. My results seem a little strange though and I'm hoping that someone can either verify or correct them. The engine drawings show that the thrust line is about .4" below the centerline between the cups on the mount, and when I relate that dimenion to the firewall it places it about 1.5" below the leveling line which is drawn. In looking at the many photos I have of completed 360's the cowl splits all seem to run inline with the split beteween the front deck and the fuselage and run in a straight line from the front of the cowl back to the canopy line. This would suggest that the thrust line is, in fact, aligned with that leveling line which was drawn on by the factory (on the fast build kit anyway.) If any of you out there are to the point where you've got your engine hanging already but still have access to that level line, could you check this for me and let me know if I'm on the right track? I'd sure appreciate it.