Return-Path: Received: from smtpa.gateway.net ([208.230.117.247]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 23 Mar 1999 19:01:57 -0500 Received: from oemcomputer (2Cust13.tnt26.chi5.da.uu.net [208.255.14.141]) by smtpa.gateway.net (8.9.1/8.9.1) with SMTP id TAA21562 for ; Tue, 23 Mar 1999 19:03:58 -0500 (EST) Message-ID: <005501be758a$5c6df800$ad3afad0@oemcomputer> From: "bobjude" To: "Lancair Mail List" Subject: LNC2 Nose Gear Door Date: Tue, 23 Mar 1999 18:07:51 -0600 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Michael Fopp, In regards to your posting about "one hose or two hoses on the nose gear door actuator"; I think you have a little different situation "In flight" than you do when ground testing your gear. When you go to lower your gear in flight, you have some air pressure trying to keep the door closed. The actuator must push against this force. Yes, currently, I believe Lancair is recommending that the second port be connected to the low pressure side of the hydraulic system. As evidence that this is probably a good idea, the next time you are around a bunch of Lancair 2 place, take a look at the top side of the gear doors and see how many have a nice arc inscribed in the paint. This is from the nose gear dragging on the door. Then look at the worst ones and see if they have one hose or two hoses on the actuator. I think you can make your nose gear drag on the door even with two hoses if you drop your gear at too high an airspeed. I have noticed a little scratch on mine even though I have the two hoses connected per the new recommendation. Bob Jude N65BJ