Return-Path: Received: from imf16aec.mail.bellsouth.net ([205.152.59.64] verified) by logan.com (CommuniGate Pro SMTP 4.2b2) with ESMTP id 3180929 for flyrotary@lancaironline.net; Tue, 20 Apr 2004 13:38:23 -0400 Received: from TOSHIBAjhr ([209.214.14.150]) by imf16aec.mail.bellsouth.net (InterMail vM.5.01.06.08 201-253-122-130-108-20031117) with SMTP id <20040420173821.XGI1714.imf16aec.mail.bellsouth.net@TOSHIBAjhr> for ; Tue, 20 Apr 2004 13:38:21 -0400 From: "John Slade" To: "Rotary motors in aircraft" Subject: Wanted - single stage turbo Date: Tue, 20 Apr 2004 13:38:21 -0400 Message-ID: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0087_01C426DC.BEECD830" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Importance: Normal In-Reply-To: This is a multi-part message in MIME format. ------=_NextPart_000_0087_01C426DC.BEECD830 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit Rotarians, Does anyone have a good second gen single stage turbo they want to sell? Failing that - can someone recommend a good supplier / rebuilder? Yes, you guessed it - I flew for almost an hour this morning, then fried the turbo. I'd noticed a bit of slack in the bearings, so was expecting to have to rebuild it anyway - just not quite this soon. The good news is that the failure mode was fairly benign. I was trying out the turbo at 5000ft and just passing through 170 kts making large circles over the field. The rpm dropped from about the 4500 I was using to 3500 and no amount of throttle would increase it from there. Below 3500 the engine ran almost normally, so I had enough power to climb if needed. It was maybe a tad rough, but not so's you'd notice. An observer says I put out a puff of white smoke, and was trailing a small amout of white smoke as I headed back in for a normal landing. In all I ran the engine for about 10 minutes after the turbo shaft broke. I lost about 1 pint of oil and the same of coolant through the collapsed bearings, so perhaps another 10 minutes or more would have been ok if the field had been further. The exhaust wheel was floating around in the wastegate housing, but too large to get through the hole, so all it did was block the exhaust a bit. I guess this is the "experimental" part of the exercise. :) John Slade Rotary Cozy IV (currently sans turbo) ------=_NextPart_000_0087_01C426DC.BEECD830 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Rotarians,

Does anyone have a good second gen single = stage turbo=20 they want to sell?

Failing that - can someone recommend a good = supplier /=20 rebuilder?

Yes, you guessed it - I flew for almost an = hour this=20 morning, then fried the turbo. I'd noticed a bit of slack in the bearings, = so was=20 expecting to have to rebuild it anyway - just not quite this=20 soon.

The good news is that the failure mode was = fairly=20 benign. I was trying out the turbo at 5000ft and just passing through = 170 kts=20 making large circles over the field. The rpm dropped from about = the 4500 I=20 was using to 3500 and no amount of throttle would increase it from = there. Below=20 3500 the engine ran almost normally, so I had enough power to climb if = needed.=20 It was maybe a tad rough, but not so's you'd notice. An observer = says I put=20 out a puff of white smoke, and was trailing a small amout of white smoke = as I=20 headed back in for a normal landing. In all I ran the engine for about = 10=20 minutes after the turbo shaft broke. I lost about 1 pint of oil and the = same of=20 coolant through the collapsed bearings, so perhaps another 10 minutes or = more=20 would have been ok if the field had been further. The exhaust = wheel was=20 floating around in the wastegate housing, but too large to get through = the hole,=20 so all it did was block the exhaust a bit.

I guess this is the "experimental" part of = the=20 exercise. :)

John Slade

Rotary Cozy IV (currently sans=20 turbo)

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