Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5.6) with ESMTP id 1130397 for rob@logan.com; Mon, 11 Mar 2002 21:59:37 -0500 Received: from mail7.carolina.rr.com ([24.93.67.54]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Mon, 11 Mar 2002 13:14:44 -0500 Received: from HappyDesktop ([24.74.32.204]) by mail7.carolina.rr.com with Microsoft SMTPSVC(5.5.1877.687.68); Mon, 11 Mar 2002 13:17:42 -0500 From: "Matt Hapgood" To: Subject: First long flight in my 360... long Date: Mon, 11 Mar 2002 13:17:54 -0500 Message-ID: <000001c1c929$10340010$6401a8c0@HappyDesktop> MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit Importance: Normal In-Reply-To: <006701c1c90c$02ec0fa0$6401a8c0@lancair.com> Return-Path: hapgoodm94@alum.darden.edu X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I haven't updated the list in awhile with 366B's progress, so here it is. After 3 months of being "down" I finally got the plane flying about two weeks ago. The plane had been down since mid-November (less than 3 weeks after getting my IFR :( ). I decided to remove the turbo charger and see what happens. Ultimately, I ended up doing the following: 1. Remove turbocharger 2. Remove cylinder head "squirters" 3. Top overhaul 4. Change to SkyDynamics sump and intake system 5. New exhaust system 6. New fuel injectors 7. Remove a "snorkel" intercooler air scoop (that was costing about 2 - 3 knots) 7. A bunch of little stuff I flew the plane about two weeks ago, and although set to a VERY rich mixture (remember this is an electronic fuel injection and ignition) the plane ran fairly well. I had a leaking governor that took awhile to diagnose, I just kept finding oil all over the place yet couldn't see a leak. That's fixed now, and in the last 8 hours of flight I have burned about 2 quarts of oil. I am still using my "old" hideous cowl. It has a snorkel scoop for the oil cooler, two big bulges for the old "tuned" induction runners, and the extraneous bottom bulge air intake - that has duct tape covering it... I have a whacked a new hole just below the prop and have a piece of 4" scat tube protruding from the cowl for the air intake now (it's so ugly you probably can't even imagine it). I flew off the 5 hours required for the change, and have taken 3 long flights - 1) Charlotte to Atlanta, 2) Atlanta to Boca Raton, and 3) Boca Raton to Charlotte. After figuring out an erratic "miss", everything has been great. Here are the details: Each of the flights was made at gross weight (1,950 pounds). Me, a 180 pound friend and about 46 to 48 gallons of fuel (not quite full). Note that the plane is heavy dry, and I have an angle valve engine and MT prop. I have been climbing about the same rate as with the turbo - averaging about 1000 FPM and 140 KIAS through to 9000 feet, at gross weight (1,950). This is climbing at 2600 RPM - the governor needs to be adjusted to get the 2700 RPM limit for this engine. I cruised at 9,000 feet at 21.7" and 2470 RPM. This resulted in KIAS of 159 and KTAS of 184. This is about 10 knots slower than with the turbo running 26" and 2400 RPM. But fuel burn is now about 8 GPH at this setting (how does this compare to others at 22" x 2450 ?). These results are while running lean of peak. The engine has absolutely no problem running LOP. I have dual EFI systems - one is set to run ROP all the time, the other is set to run LOP while in the range of 2100 RPM to 2500 RPM. It works incredibly well now - but the amount of time to get it set up has been incredible, and I think there is still some improvements that can be tweeked from the system (for instance, I am only running 23 degrees of advance at the above listed power setting, vs the factory spec of 25 degrees). Other details for the return trip (Boca to Charlotte): Total distance 566 NM Total time enroute 3:31 (fighting a vicious headwind, as much as 46 knots in SC) Fuel burned 29.5 gallons Fuel remaining 18.4 gallons Average GS 160.4 knots Typical KTAS 184 Density Alt 10,200 Temperatures: OAT 58F Oil Temp 172 (pressure 86) Cyl 1: 292 / 1454 Cyl 2: 292 / 1444 Cyl 3: 318 / 1462 Cyl 4: 292 / 1454 I have a new cowl that I hope to get on the plane some time in the next week. I am optimistic that I will then be able to cruise 195 knots LOP at 9,000 feet burning 8 to 8.5 GPH. Any thoughts? The trips were all great - I was finally able to use the plane for its intended purpose. It was so comfortable during the trip, I was thrilled. Some light IFR during the trip to Boca, other than that beautiful weather too. The S-TEC 30 ALT autopilot, coupled with the Sandel EFIS, was also great. I did not have to do anything other than monitor and climb / descend. Each waypoint was smoothly transitioned to the new heading with no input from me. That's all, I think I'll go flying now... Matt >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>