Return-Path: Received: from quackerjack.cc.vt.edu ([198.82.160.250]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 6 Jul 1999 10:56:13 -0400 Received: from sable.cc.vt.edu (sable.cc.vt.edu [128.173.16.30]) by quackerjack.cc.vt.edu (8.8.8/8.8.8) with ESMTP id KAA14060 for ; Tue, 6 Jul 1999 10:59:22 -0400 (EDT) Received: from [128.173.82.25] (tracyw.biotech.vt.edu [128.173.82.25]) by sable.cc.vt.edu (8.8.8/8.8.8) with ESMTP id KAA16499 for ; Tue, 6 Jul 1999 10:59:21 -0400 (EDT) Message-Id: In-Reply-To: <19990704042043.AAA5387@truman.olsusa.com> Date: Tue, 6 Jul 1999 10:59:30 -0400 To: From: Tracy Wilkins Subject: Re: posting to list X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> We are new to the list and purchased our Lancair 360 a year ago with 100 hrs. We just tore it apart for our first annual and rebuilt a lot of things with our local certified mechanic and avionics guys..... Perhaps our experience can be helpful to builders... 1. We have never had any nose wheel shimmy problems (plane was finished in 95). 2. We did have a lot of electrical connection problems and I urge builders to pay close attention to that area - eventhough it is almost the last thing and you want to get in the air! Don't use spade fittings unless you have too - use round ones over every screw. Solder to make the connections. Ground it several places. Until we did that our Vision Microsystems instruments were varying all over the place. The manifold pressure was useless and rpm fluctuated etc in high humidity. All of it was due to bad connections. 3. We also moved the circuit breaker for the hydraulics up front where it belongs instead of back next to the pump.. Also put in an idiot light to warn of alternator failure(Spruce Co.)- after the alternator failed and I didn't notice anything until I had a brownout in the air! We also need a bigger alternator than the 35 amp job we have but don't have much room - any ideas?? 4. One major screw-up - the avionics were all on their own busbar with a switch = great. Except that that bus bar actually was part of the main bus bar structure, and somehow during the annual (at about 250 + hrs) we broke the bus bar between the avionics and master. That made some things touch that shouldn't have and on start up we toasted the entire avionics stack with super high voltage with the avionics master in the off position! The main radios had protection diodes that protected them somewhat but the audio panel actually blew up and smoked. The transponder was a $450 redo and the encode was toast.... We recommend separating the avionics bus bar from the master bus bar with some space! 5. Also it got real hot in the plane in the summer so we put in large "black ball" type nozzels (Spruce again) directly on the air inlet scoops - works great. The 3/4 inch tubing leading to the nozzles on the panel never gave enough air; now we have to turn the air flow down. 6. The 360 overheated last year in the summer (450+ and climbing on #3 cylinder on take off. Thats the back cylinder on the pasenger side). We have helped that a lot with fanatical attention to the fit between the cowling and the baffles - we changed to the red silicone rubber baffling material and worked hard to get a perfect fit. We also used a lot of tubes of the red engine caulking to stop up even the smallest holes - we wanted all the air to go around those cylinders. Seems to be working. 7. We had two leaks with the header tank - first one was there when we got it - the canopy was putting pressure on the seal when the canopy was in the full up position (the hinge was contacting the header tank). Fixed that by pulling a vacuum on the header tank with a vacuum cleaner and sucking epoxy into the crack - then added some reinforcing fiber glass to protect that area - solved the problem so far but we are careful not to let wind blow the canopy forward and put too much pressure on the seal. Second leak happened when we put new half inch black insulation on the firewall. We got this too close to the header tank so that when we tried to put it back on we "had" to use some pressure on the sides to make the piano hinges get in line. That sprung the seal in another place - fixed it the same way. 8. The sight tubing for the header tank fuel level was clear plastic but it had gotten hard and brittle - Lancair said to replace it with yellow tubing that is supposed to resist gasoline much better. We did- now we have trouble seeing the fuel level in some light conditions. Seems like we need a small colored float on the top of the gas inside the tubing??? 9. The battery was installed where the rudder pedals would normally be on the passenger side. The buliders did this because this was one of the first kits with the new big tail and when they put the battery in the back, it put the CG out of whack. We would like to move it but the CG calculations do not work out - we would have to add 20 - 30 lbs of weight somewhere in the engine compartment area. Having the battery under your feet restricts us to carrying short people like us (but the tall guys got the play basketball so why should they have all the fun....) Any of you guys have this problem with the battery??? 10. Also had a problem with the axels on the mains - they allowed the tire to move back and forth sideways - the mechanic finally got new axels from Lancair that fixed the problem - Matco was no help... 11. We replaced all the hydraulic hoses - Lancair now uses better quality than was on our plane. We had a couple of seaping leaks before. Tracy Wilkins Director of Biotechnology Va Tech, Blacksburg, Va 24061 540-231-6935 231-7126 FAX >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html