Return-Path: Received: from lanfear.nidlink.com ([216.18.128.7]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 9 Oct 1999 09:52:23 -0400 Received: from enaila.nidlink.com (root@enaila.nidlink.com [216.18.128.8]) by lanfear.nidlink.com (8.9.0/8.9.0) with ESMTP id GAA13655 for ; Sat, 9 Oct 1999 06:56:25 -0700 (PDT) Received: from regandesigns.com (tnt132-91.nidlink.com [216.18.132.91]) by enaila.nidlink.com (8.9.0/8.9.0) with ESMTP id GAA25312 for ; Sat, 9 Oct 1999 06:56:19 -0700 (PDT) Message-ID: <37FF4944.881E8633@regandesigns.com> Date: Sat, 09 Oct 1999 06:55:17 -0700 From: Brent Regan To: Lancair List Subject: Re: Hydraulic Flap Cylinder Throw LNC4 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Dave is right that the flap hydraulic cylinder should be rigged to allow the piston to bottom at both ends of it's stroke. The Fowler bracket and flap pushrods should not provide the end of stroke limits. In order for the two flaps and hydraulic cylinder to be coordinated, they must be rigged properly. In a bellcrank system, the stroke ratio between the driver and driven pushrods is not always 1:1 (assuming equal length arms). This ratio can be adjusted by lengthening one pushrod while shortening the other, effectively changing the position and cord length of the swept arc of the bellcrank. All 5 bellcranks must be adjusted together to achieve symmetrical and complete deployment of the flaps without binding the system at the ends of stroke. This is not an easy process as there are an infinite number of ways to set them incorrectly and only one right way. It took me a day and a half, not including several breaks to let my blood pressure settle back into the green. The problem I had was getting enough flap deployment so if the factory had supplied a shorter cylinder, my airplane would have been more difficult to rig. My advice is to make a chart of the system, measure and record the initial lengths, make a change and record the results. This way you can see trends and follow them. I am unaware of any universal method for adjusting the flap system as every one is slightly different due to building variances. If all else fails (your as built dimensions are outside the limits of adjustment), then machine a spacer (fat washer) for inside the shaft end of the cylinder. It is apparent from David's post that his flaps are not symmetrically rigged as only one pushrod on the left side bent indicating that it was the first to reach it's limit by enough of a margin to allow it to bend. It has been a while since I reviewed my manuals, but there isn't a caution about proper flap rigging, there should be. The aileron system has a similar rigging requirement. I found that having two digital inclinometers (one on each aileron) was very helpful in getting them set properly. Curiously, rigging an aircraft requires a similar mindset to setting up the suspension in a race car. If you don't have a buddy that is familiar with AC rigging then a race car mechanic would be my second choice. Regards Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html