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, 27 Nov 1999 12:19:26 -0500 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 JAA29396 for ; Sat, 27 Nov 1999 09:23:58 -0800 (PST) Received: from regandesigns.com (tnt132-34.nidlink.com [216.18.132.34]) by enaila.nidlink.com (8.9.0/8.9.0) with ESMTP id JAA14493 for ; Sat, 27 Nov 1999 09:23:56 -0800 (PST) Message-ID: <38401340.79A1DE3D@regandesigns.com> Date: Sat, 27 Nov 1999 09:22:09 -0800 From: Brent Regan To: Lancair List Subject: Static Water X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> The other day we had a patch of blue sky pass overhead (the first in two weeks) and my thoughts turned to flying. My two sons wanted to go as well so we preflighted the IV and piled in for a pleasure flight. Just before Vr I noticed that the airspeed was about 5 Kts fast, the pleasures of winter's density altitude I thought. On climb out my scan caught the altimeter, VSI and airspeed needles all jump simultaneously. I leveled off at about 1500 AGL and brought the power back to 18 inches. Holding it level I was indicating 220 Kts, then suddenly 180 Kts. Not good. It was obvious from the symptoms. The patient had enough water in its static system to occlude the line and the needles would jump whenever a bubble would pass. All the static instruments were affected including VSI, airspeed, altimeter, encoder, cabin altimeter, AOA and my RMI backup. I couldn't trust any of them. Even the GPS altitude readout is affected by the encoder. What was left isn't really needed on a VFR flight. I have two static ports but no alternate static source (pressurized cabin and all). OK, here is the plan: proceed to COE, get AWOS, use GPS plus wind component to estimate airspeed, stay high and hot and follow the ILS to a happy ending. Why not just land the damn thing? you ask. Well, I believe in using all available information and I don't like taking any chances in the pattern. Only one problem with "The Plan", a message at the end of the AWOS states that the runway with the ILS (5) is closed. My options are now to either land on 1 (crosswind, 2000 feet shorter, no ILS) or land on 5 anyway. I decide I need more information and make a low pass over 5. Everything seems normal and sometimes the airport manager forgets to change the AWOS message after they do maintainance, so runway 5 it is. Safety is greater than rules. After an uneventful landing I taxi over to the fuel island and shut down. I disconnect the static line under the instrument panel and then I get out and proceed to suck the water out of the static system. This prompts my 6 year old to query "Dad, how come you are kissing the airplane?" After I stop choking I explain what I am doing. I suspect he is not convinced. So how did this happen to a pampered, always hangered airplane? Well, since the last flight, I had the concrete floor in the hanger sealed so I had to park the bird outside (gasp) overnight. That night was windy with a light rain. As I mentioned I installed two static ports, one on each side, that are "T"ed together. The wind must have created a pressure differential between the ports that sucked in about 10cc of water. The same conditions have existed at OSH but the colder temperatures here prevented the water from evaporating. Check those static lines!! Compliments of the season. Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>