Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 28 Jun 2002 19:09:07 -0400 Message-ID: X-Original-Return-Path: Received: from siaag2ad.compuserve.com ([149.174.40.134] verified) by logan.com (CommuniGate Pro SMTP 4.0b4) with ESMTP id 1516381 for lml@lancaironline.net; Fri, 28 Jun 2002 17:09:25 -0400 Received: (from mailgate@localhost) by siaag2ad.compuserve.com (8.9.3/8.9.3/SUN-1.12) id RAA23544 for lml@lancaironline.net; Fri, 28 Jun 2002 17:09:26 -0400 (EDT) X-Original-Date: Fri, 28 Jun 2002 17:08:03 -0400 From: James Frantz Subject: [LML] Re: stall/spin X-Original-Sender: James Frantz X-Original-To: "INTERNET:lml@lancaironline.net" X-Original-Message-ID: <200206281708_MC3-1-458-7A7B@compuserve.com> MIME-Version: 1.0 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline < if there is ONE trend I've seen among the "high = HP" crowd it's this: a woefully inadequate use of rudder during large power = changes - particularly evident during go-arounds, missed approaches, and the = like. Deadly if you happened to be nearing the stall due to that increas= ed bank angle. (Stall+Yaw=3DSpin ---> more altitude than you have, if you'r= e in the pattern!)< I second the comment above. It is great to see a Lancair rep. talking about the importance of rudder as opposed to the "you need never touch th= e rudder" sales statements of past years. The fact is that lots of right rudder is required at high power settings when accompanied by higher AOAs= . = Sport aircraft are running nearly double the fatalities due to stall spin= s as compared to Part 23 certified aircraft. The reasons are many but may include: 1. Experimentals are not stall certified 2. Experimentals are not required to have active stall warners 3. Experimentals are not required to have the higher stability as require= d on Part-23 aircraft 4. Experimentals are not certified spin resistant 5. Lancairs cruise faster which equates to higher stalling speeds 6. Higher powered singles generally require more rudder than their underpowered sisters. I hope that we can all agree that practicing recoveries from APPROACHES t= o stalls is a very good thing. After all, this training is required for al= l pilots by the FAA. However, practicing recoveries from FULL stalls may b= e a good or bad idea depending upon the aircraft type, CG, GW, and pilot experience. I also hope that we can all agree that practicing spins in Lancairs would= be unwise unless we are prepared to loose our aircraft, are wearing a parachute and have a way out. Besides it is in violation of FARs without= the parachute. If we agree on this point, then we must conclude that not= all aircraft are ideal for practicing FULL stalls because some lack spin= resistance and well behaved spin characteristics . I must say, suggesting the requirement that we all explore the extremes o= f our aircraft is bordering on irresponsible. We have enough insurance problems without this poppycock. James B. Frantz Proprietary Software Systems, Inc. = www.angle-of-attack.com LFrantz@compuserve.com (952) 474-4154