Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Mon, 31 May 2004 16:38:36 -0400 Message-ID: X-Original-Return-Path: Received: from [68.168.78.44] (HELO mta13.adelphia.net) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP id 98337 for lml@lancaironline.net; Mon, 31 May 2004 16:33:43 -0400 Received: from f3g6s4 ([69.166.117.156]) by mta13.adelphia.net (InterMail vM.5.01.06.08 201-253-122-130-108-20031117) with SMTP id <20040531203313.PLD13425.mta13.adelphia.net@f3g6s4> for ; Mon, 31 May 2004 16:33:13 -0400 X-Original-Message-ID: <003e01c4474e$8b63a100$9c75a645@losaca.adelphia.net> From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: Re: lnc2 flaps X-Original-Date: Mon, 31 May 2004 13:33:33 -0700 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1409 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 Per Gerard's question about the flap actuation: Can't comment on the need for bushings since I have an early 235 version and I think the flap mechanism on later models was changed. However, I believe the same (or similar) actuator was used (magnetically operated limit switches). Early on, I had some trouble with the actuator getting beyond the up-limit switch allowing the motor to drive the to the mechanical stops, resulting in the mechanism jamming in the reflex position. This happened several times, most of which was caught during the pre-flight check - but not every time (makes for an exciting landing if your intended runway is on the short side! Because of this, by the way, I occasionally practice approach and landing with the flaps in reflex - just in case - since anything can fail). Each time, after disconnecting the actuator from the flap lever to get things un-jammed, I found that the switch was OK. Long story short, I found that if I let go of the flap switch just before the actuator was stopped by the limit switch, the motor could coast just enough to go past the point where the limit sw. should have stopped it. I believe the magnetized portion of the feed-back rod is quite narrow and, in the right circumstances can get past the limit switch. In flight, and particularly during the initial flight test period, this would happen when I "milked" the flaps into reflex, trying to find the best amount of reflex. I never had a jam when I just held the flap switch until the limit switch stopped the motor. As an aside, I didn't like this and designed a separate flap drive limiting device that is not affected by motor "coast". It also allows selecting any amount of flaps without looking out at the wing to see where the flaps are (really helps on a go-around). Pretty easy to build and I think the plans are in Marv's archives. Dan Schaefer