Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.7) with ESMTP id 793160 for rob@logan.com; Thu, 31 May 2001 10:59:47 -0400 Received: from granger.mail.mindspring.net ([207.69.200.148]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Thu, 31 May 2001 10:22:15 -0400 Received: from edechazalmindspring (user-2injklf.dialup.mindspring.com [165.121.210.175]) by granger.mail.mindspring.net (8.9.3/8.8.5) with SMTP id KAA02416 for ; Thu, 31 May 2001 10:29:44 -0400 (EDT) Message-ID: <015201c0e9d5$b6706920$1bd079a5@com> From: "Ed de Chazal" To: References: <20010530044133.AAA20110@pop3.olsusa.com> Subject: Re: LNC2 100 hour report Date: Thu, 31 May 2001 09:28:49 -0400 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I figure some of you might be interested in how things look on my 360 at the 100 hour mark. I've been flying it for 9 months now and have made a number of long trips. It is still in the debug stage (if that ever ends) and paint is scheduled for late June. The engine (IO360 B1F) has proven flawlessly reliable and has not been affected by the recent crankshaft and fuel pump advisories we've seen. Temperatures: The CHTs are coming down now after some cowl tweaking and takeoff technique changes. They were crowding 450 degrees on warm air takeoff and 400 degrees at cruise when leaned beyond 150 degrees rich of peak. Cylinder #3 is the hottest. My oil cooler is in front of number 2 and my filtered air intake is in front of number 1. To improve things, I've added ramps inside the upper cowling to smooth the inlet air. I've also capped the cabin heat valve on the exhaust side so that air no longer is robbed from behind cyl. 3 unless it's cold outside. At takeoff, I now open the ram air inlet which cuts the draw from in front of cyl 1 and increases power substantially. The combined affect is to lower takeoff and climbout CHTs to below 410. Cruise CHTs did not seem to be affected much. Next, I've added more silicone around the baffling and have installed exit air down ramps at the bottom of the cowl using bent aluminum sheetmetal pop riveted in place. My initial test shows that I can now lean to 50 degrees ROP (the hottest CHT situation) and be at 375 CHT (zero degrees ambient at 10k feet 75% (2500 rpm, 21.4 inches) power). That's a 30 to 40 degree improvement over before at cruise. These exit air ramps are sheet metal flanges that bend down at about a 35 degree angle and are 1 inch long after the bend. There are 3 of them, one in front of the nose gear slot (3 inches wide) and one on either side of the nose gear at the back of the cowling (6 inches wide each). So it appears that I have the cooling licked but their seems to be a slight penalty on speed: 191 kts at the same conditions above. High Speed Vibration: There is a noise that comes in at around the top of the green arc usually during descent. I estimate that it's around the 100 Hz range, maybe lower. It's heard (Bose headsets), not felt and it was NOT there on day one. I suspect gear doors/wells as the culprit since the mains are not very flush yet and there are gaps where air can see into the well. Also the nose door has relaxed away from the fuselage in the rear 3rd of the door. I build this peice on the flat bench and tried to heat bend it but I think with the exhaust heat it goes back to its original shape. I'll next remove bid and foam, bend it, then install new glass to lock in the desired shape. Also, I've yet to install the nose gear close out that seals the leg to the sheet metal boot. I've had "creaking" in the gear while taxiing. While it sounds like something is cracked, the springs just needed some grease. I had a nose gear tire go flat at the far end of my home runway. Happened all of a sudden. Memo: always carry at least a spare inner tube since no FBO has the tiny 4 series tires/tubes. The brakes do not hold the plane still at 1800 rpm runup (MT prop). Don't yet know for certain if it's the tire skidding or not enough brake. In any event, too much leg power is needed. I have the original pads on from 5 years ago and will try the replacement Cleveland pads I received. Rain: OK, I now believe it. Rain is like shot peening. Any week spots in the skin like poor primer adhesion along the leading edges or foam buildups around the cowl inlets not glassed over will erode. I made the apparent mistake of not glassing over my carefully micro and foam contoured surfaces on the cowl and elevator counter weights. These will now have to be glassed if they are to survive. The leading edges appear to be fine except for random locations on the wings. Make sure to take a garden hose to your plane early on so that you can see how water tight it is. Take the seats out first. Mine fills with water in the seat area! I thought it was the untaped D section but now I'm certain it's coming from the outback flap torque tube openning. Unfortunately, water channels right to this area and in my case I had to cut away some of the top flap skin for clearances. Factory says a boot over the torque tube won't work so I'll close out the tube with some plates of one sort or another. What's worked great: Automatic fuel trasfer system between wings and header. Ground power outlet underneath the door handle. Hydraulic gages on panel. Bose headsets are great and music comes through as if at home. The portable CD player plugs into a jack on the panel. I've got 2 power outlets at the bottom of the pedestal, one for CD player, one for the Garmin 295. Fuel tank sealer inside the cabin anywhere hydraulic oil might spill. Makes a clean appearance and helps you keep things clean. Forget about co-pilot rudder pedals unless you really think you need them. I don't have them and put the space to good use. The mountain high Oxygen system (EDS system with kevlar bottle) is great. I really feel the difference after a cross country and the cannula does not interfere with the headset. It opens up another set of altitude choices. What's not great: When you are strapped in, you can't reach far. The eyeball vents for fresh air are in plans location and unreachable. Scott Krueger showed me a neat stick he uses to reach them. I wish I had electric rudder trim. I'd rather have a Garmin 430 in the panel. The one touch up flap relays were a waste of time: I found a switch that does exactly the same thing: middle position is off, spring loaded return from the down position but detented up position. Gear Minder was a waste unfortunately since there seems to be a software bug and I had to bypass it. I'm having a devil of a time sealing the canopy. The plans glove box was a waste because I need that surface to mount the portable GPS. I use pockes for pencils. Get the nice static ports from aircraft spruce so that your static integrity is not subject to how well you bond fittings into the skin. My only leaks were at both ports until I switched. My plane fits people 6 feet tall and smaller. A lot of your friends are taller than 6 feet zero inches so plan for that while you still can. Don't put the gear switch anywhere close to the flap, trim or anyother switch you grab during the checklists. It's a damn accident waiting to happen. I moved mine from the pedestal to above the flight instruments. Get your trim and flap indicators in easy view. You only need the trim indicator prior to takeoff but you need your flap indicator in the pattern. Mine were hidden by the engine controls. The inboard gear doors flap in the prop wash on the ground (outback gear). Best I can tell it's mostly a function of sloppy hinge pin fits. I think there's a nylon sleeve that can be used, can anyone confirm? The plane is fun to fly: 150 kts and 1000 fpm on climbout and it will maintain 1000 fpm beyond 10k feet indicating 135 kts (all stock stuff but with ram air and at 1650 lbs). You can get astronomical climb rates (2000 fpm at 120 kts) but the deck angle is extreme and not practical. Happy Flying, Ed de Chazal, Rochester Michigan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>