Return-Path: Received: from hpamgaab.compuserve.com ([149.174.217.153]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sun, 23 May 1999 01:35:11 -0400 Received: (from mailgate@localhost) by hpamgaab.compuserve.com (8.8.8/8.8.8/HP-1.4) id BAA12593 for lancair.list@olsusa.com; Sun, 23 May 1999 01:37:53 -0400 (EDT) Date: Sun, 23 May 1999 01:36:42 -0400 From: Rick Argente Subject: Aileron Vibration Sender: Rick Argente To: "lancair.list@olsusa.com" Message-ID: <199905230136_MC2-76C1-94C6@compuserve.com> Mime-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline X-Mailing-List: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> So far, I have about 10 hours on N360ZR. I have a couple of small bugs to sort out here and there but one nagging problem I have is the left aileron, it vibrates! The right aileron looks quite solid looking out from the canopy but the left has this small up and down vibration which can be felt on the control stick. Part of the vibration is probably being transmitted from the engine/prop but I'm not sure. I will have to prop dynamically balanced next week and will also install the new engine isolators. Here are the facts: 1 . It vibrates at both high and low speeds, more vibration at higher speed, less at lower speeds. 2. The vibrating aileron has a mac servo inside for the trim tab (piano hinge tab). 3. The aileron control system has almost zero slop, it is quite tight and no binding whatsoever. 4. Both ailerons are over 100% balanced but the trailing edge of the right aileron moves UP MORE (about 1/4") when hanging from the hinges, detached from the control rods. The left aileron only moves up about 1/8" inch. 5. Yesteday, at around 160 knots IAS, it applied full left trim and held the stick at neutral, the vibration ceased. So, loading up the aileron stops the vibration but I don't know what that means exactly. 6. The top skin of the right aileron is flushed to the top main wing skin throughout the aileron span. But the middle portion of the left aileron has a small dip. The dip is about 1/16" wherein the aileron top skin is lower than the wing skin. Can't remember exactly how wide the dip is but I will estimate a around 5". I'm wondering if air flow is somehow broken here and causing the vibration. I added more weights to the left aileron to equal the 1/4" over-balanced condition of the right aileron. Haven't flown yet since this mod. If that doesn't reduce or eliminate the vibration, I plan to eliminate the middle dip of the top skin of the left aileron by increasing the thickness of the skin using some duct tape temporarily. I'm kinda of running out of ideas and don't really know if what I'll be doing will help any. Any other ideas out there?? Please feel free to voice them out as I'm getting a bit frustrated. Oh yes, another thing, during one of our flights, the CHT's reached 450-degrees during initial climbout with full power, @120 knots. I thought that the CHT problem has been solved but I guess not. It's getting warmer here now, much warmer than when we first did the inital test flights, around 75 to 80 degrees. I am contemplating on adding another vent hole at the bottom of the cowling to increase exit air volume. Any other ideas on how to reduce my CHT's. Oil temps are at 170 degrees. Thanks Rick Argente N360ZR >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html