Return-Path: Received: from [65.33.162.162] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.2b3) with HTTP id 3231843 for lml@lancaironline.net; Thu, 13 May 2004 23:52:59 -0400 From: "Marvin Kaye" Subject: Re: Lancair vid To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.2b3 Date: Thu, 13 May 2004 23:52:59 -0400 Message-ID: In-Reply-To: <20040514004504.91633.qmail@web60701.mail.yahoo.com> References: <20040514004504.91633.qmail@web60701.mail.yahoo.com> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit [This is a message I received a short while ago from Dave Allen. The video clip he mentions has been uploaded to the LML website.. go to the bottom of the "Finished Aircraft" page in the Attachments area. ] Posted for David Allen : Hi, I am surprised at the response to my video and web site. I've had many emails and my web site has been overwhelmed. I have since upgraded my site to handle the extra volume. It may not be fully implemented for a day or two. I'm attaching a few seconds of my video that is available from me for $30. Hopefully you can load it onto a server for me. This is an inadvertant spin. This is supposed to be a deep stall with a 1/2 turn spin. The Lancair went around about 3 turns. I had done many stalls and deep stalls and deeper stalls/spin entries leading up to this and the aircraft behaved normally. On this flight we had moved the CG back from the front part of the envelope, but not yet half way back. I was doing my utmost to recover by 1/2 turn, which for most airplanes is quite easy, and it went around 3 times and lost 1500+ feet. I started this at 11,500 ft and was wearing a chute. I would have bailed in about 2 more turns.... We terminated stall testing at this point and declared intentional spins a prohibited manuever. I was aware of the reputation of these airplanes, but all stalls leading up this were normal (CG forward, stalls, 1/4 turn left, 1/4 turn right, 1/2 turn left, 1/2 turn right). It is my belief that if you stall these planes with some yaw, with the CG in the middle or aft, it will enter an unrecoverable spin. Be careful with your flight testing or hire a pro! How many builders who do their own flight testing perform stalls at max gros weight and aft CG? How many pull max allowable G's at max weight? How about negative G's. If your planes entire allowable envelope hasn't been experienced, then the flight testing isn't complete. Dave at daveandjj@hotmail.com www.geocities.com/daveandjj