Return-Path: Received: from web118.yahoomail.com ([205.180.60.99]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with SMTP id com for ; Sat, 10 Jun 2000 12:13:07 -0400 Received: (qmail 23758 invoked by uid 60001); 10 Jun 2000 16:19:05 -0000 Received: from [167.154.3.19] by web118.yahoomail.com; Sat, 10 Jun 2000 09:19:05 PDT Message-ID: <20000610161905.23757.qmail@web118.yahoomail.com> Date: Sat, 10 Jun 2000 09:19:05 -0700 (PDT) From: Jerry Conners Subject: Lancair 235 Spin Recovery Procedure To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Does the Lancair 235 have adequate rudder authority to recover from spins? Anyone having performed spin recovery in this aircraft, please provide a description of the manuever and a description of remaining rudder movement available during the recovery. Jer ===== Jerry L. Conners, PE Civil Engineer [There was a pretty lively discussion of this topic here awhile back. If you search the archives for "spin" you'll find some very useful information on that topic. ] >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>