X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 26 May 2008 00:32:22 -0400 Message-ID: X-Original-Return-Path: Received: from yw-out-2324.google.com ([74.125.46.29] verified) by logan.com (CommuniGate Pro SMTP 5.2.3) with ESMTP id 2937744 for lml@lancaironline.net; Sun, 25 May 2008 09:00:12 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.46.29; envelope-from=ronlaughlin@gmail.com Received: by yw-out-2324.google.com with SMTP id 3so926457ywj.7 for ; Sun, 25 May 2008 05:59:26 -0700 (PDT) DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=message-id:date:from:to:subject:in-reply-to:mime-version:content-type:content-transfer-encoding:content-disposition:references; b=ivboXrvdN7ly/XP90E8T7JjsCorv6zATgOvJBqcQBVTNBU6J1asdt/IEDCy8OpVKXvZ6p/hZ3BVnQoQLcCtTaxxuaE7DQpqFnVUqtiRkjx5WdhYl0xVQA39WiEhNp4E5mP9zS7ZajTAO7YGrn+H4a989Yqw2MG9Rv6REfk/gdSI= Received: by 10.150.82.10 with SMTP id f10mr2202407ybb.144.1211720366428; Sun, 25 May 2008 05:59:26 -0700 (PDT) Received: by 10.150.215.7 with HTTP; Sun, 25 May 2008 05:59:26 -0700 (PDT) X-Original-Message-ID: <6412e9f20805250559i6b1877a7ta6de5aa496c48b27@mail.gmail.com> X-Original-Date: Sun, 25 May 2008 07:59:26 -0500 From: "Ron Laughlin" X-Original-To: "Lancair Mailing List" Subject: Re: [LML] Crankcase pressure=OIL ON BELLY In-Reply-To: MIME-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable Content-Disposition: inline References: Hi Steve, Could you post some pictures of your breather hose routing. Especially the end of the breather tube/hose where it exits the cowl. Ron Laughlin On 5/25/08, Steve Colwell wrote: > > > > My Cont. IO-550 (normally aspirated, stock comp ratio) is blowing enough > oil from the crankcase breather to put a thick coat on =BD of the belly, > halfway to the tail in 10 min. of flying. Originally I thought I had > overfilled the 8 qt. crankcase so I drained the oil, changed the filter a= nd > refilled with 6.5 qts. During runup and takeoff roll the manometer (tapp= ed > into the crankcase vent about the mid-point of its length) will read zero > until plane has about 120 knots indicated airspeed. At 120 to 200 knots = the > manometer reads 4" to 5" with a short spike up to 14" to 20" when power i= s > reduced in the pattern. The following tests have been run: > > > > Compression test: high 60's to low 70's which I am told is normal for > Continentals, oil is normal color (not black, which would indicate blow-b= y) > > > > Washed engine with mineral spirits to see if any fresh oil was appearing. > > > > Upper plugs are normal color, maybe a dark tan insulator, no fouling > problems > > > > Low pressure on crankcase with 12" balloon on crankcase vent: takes abou= t 3 > min to deflate, tried soap suds around all accessible seals, dipstick cap= , > mags, pushrod tubes, etc.. > > > > Relocated crankcase vent to right side cowl outlet > > > > Cut a anti-siphon hole 6" above the end of the vent tube on normal left s= ide > exit. > > > > Taped the dipstick cap with aluminum tape. > > > > Put 20 psi air pressure on crankcase, soap suds again, air going past pis= ton > rings, tried turning prop with no noticeable difference from cyl to cyl. > > > > Replaced crankshaft seal. > > > > Anything that required a flight test would deposit the same thick coat of > oil on the belly in a single trip around the pattern. I have just about > run out of ideas, the engine builder has never heard of anything like thi= s > and the cylinder supplier could only suggest it could be the crankshaft > seal. It could be a leaking seal in the alternators or mags or ???? = I > need help. > > > > Steve Colwell Legacy 916 505-6099 > > > > > > > > --=20 Ron Laughlin