Return-Path: Received: from dskfw1.funb.com ([168.175.254.61]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 12 Mar 1999 09:32:30 -0500 Received: (from uucp@localhost) by dskfw1.funb.com (8.8.5/8.8.5) id JAA29687 for ; Fri, 12 Mar 1999 09:34:22 -0500 (EST) Received: from clt-msw-02.funb.com(168.175.76.95) by dskfw1.funb.com via smap (V2.0) id xma029628; Fri, 12 Mar 99 09:33:55 -0500 Received: from clt-conn-02.capmark.funb.com (unverified) by clt-msw-02.capmark.funb.com (Content Technologies SMTPRS 2.0.15) with ESMTP id ; Fri, 12 Mar 1999 09:31:24 -0500 Received: by clt-conn-02.capmark.funb.com with Internet Mail Service (5.5.2448.0) id ; Fri, 12 Mar 1999 09:33:38 -0500 Message-Id: <593B00964734D111B9130000F804651C01FEF63C@CLT-EXCH-05> From: "Hapgood, Matt" To: "'Doug Waddingham'" , Lancair List Subject: RE: Gear shocks Date: Fri, 12 Mar 1999 09:33:56 -0500 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> > While I'd like the soft landing these shock absorbers are > likely to provide I'm also concerned that I'd be risking a bent prop. Am > I needlessly worrying here? > Doug Doug, I think you would REDUCE the risk of a bent prop. If the main gear compresses more, and the nose gear compression rate hasn't changed, then the nose of the plane will rise. Matt