Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.2 9/18/84; site bmcg.UUCP Path: utzoo!watmath!clyde!burl!ulysses!mhuxr!mhuxn!ihnp4!qantel!hplabs!sdcrdcf!sdcsvax!bmcg!fredc From: fredc@bmcg.UUCP (Fred Cordes) Newsgroups: net.aviation Subject: re:re:spins Message-ID: <1841@bmcg.UUCP> Date: Tue, 3-Sep-85 11:41:06 EDT Article-I.D.: bmcg.1841 Posted: Tue Sep 3 11:41:06 1985 Date-Received: Sun, 8-Sep-85 05:07:17 EDT Organization: Burroughs Corp. ASG, San Diego, CA. Lines: 7 orry about that last. The main point is that 40 degres flaps on a C150 supposedly blocks the tailplane and can cause loss of control authority. If this is combined with slow approach speed (close to stall) and cross control for a slip, a disastorous spin entry can occur, with an inverted roll entry. Fred Cordes