Return-Path: Received: from csimo01.mx.cs.com ([198.81.17.74]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 28 Jun 1999 08:20:06 -0400 Received: from RicArgente@cs.com by csimo01.mx.cs.com (IMOv20.21) id fQKMa06216 (533); Mon, 28 Jun 1999 08:23:00 -0400 (EDT) From: RicArgente@cs.com Message-ID: <68db33af.24a8c324@cs.com> Date: Mon, 28 Jun 1999 08:23:00 EDT Subject: Re: AOA Landings To: LFrantz@compuserve.com, lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In a message dated 6/27/99 3:19:29 PM Eastern Daylight Time, LFrantz@compuserve.com writes: << Actually we do have a squat switch of sorts built into the software of the AOA. What do you need the squat switch for? Are you looking for a way to prevent accidental gear retractions on the ground? >> Yes, and if you could incorporate this in your AOA product, it would be the best of both worlds. You see, I'm deciding on whether to get Lancair's gear minder system, which also includes a squat gear function -OR- your AOA / gear minder system. My decision would be a lot easier if you can add a squat gear function also! You are probably right that my pitot/static system has some sort of error at slow speeds. Yesterday, we did some slow flights with two people and approximately half fuel. The IAS was at 60 knots (no flaps, no gear), and is was only starting to buffet a bit. I added a small amount of flaps, and the buffet disappeared. <> Please give the squat switch idea some thought and consideration... Rick PS I know that the pressure sensors and water drain will be installed near the wing tips. What kind of sending medium will go from the wing tip to the cockpit, wires or tubes? >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html