X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Sun, 13 Aug 2006 19:16:13 -0400 Message-ID: X-Original-Return-Path: Received: from smtp.mailix.net ([216.148.213.132] verified) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTPS id 1321124 for lml@lancaironline.net; Sun, 13 Aug 2006 19:03:58 -0400 Received-SPF: pass receiver=logan.com; client-ip=216.148.213.132; envelope-from=jtrepicone@trepicone.com Received: from [65.60.140.48] (helo=jenny) by smtp.mailix.net with asmtp (Exim 4.24-CA) id 1GCOz7-0005HQ-LU for lml@lancaironline.net; Sun, 13 Aug 2006 16:03:09 -0700 From: "Joe Trepicone" X-Original-To: "'Lancair Mailing List'" X-Original-Date: Sun, 13 Aug 2006 19:03:12 -0400 X-Original-Message-ID: <001801c6bf2c$a73df6c0$308c3c41@jenny> MIME-Version: 1.0 X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.6626 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 X-SA-Exim-Mail-From: jtrepicone@trepicone.com Subject: RE: [LML] Re: 4 pt speeds Content-Type: multipart/alternative; boundary="----=_NextPart_000_0019_01C6BF0B.202C56C0" X-SA-Exim-Version: 3.1 (built Thu Oct 23 13:26:47 PDT 2003) X-SA-Exim-Scanned: No; Unknown failure X-uvscan-result: clean (1GCOz7-0005HQ-LU) This is a multi-part message in MIME format. ------=_NextPart_000_0019_01C6BF0B.202C56C0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable I don't think anyone can answer this question at the moment although I understand it's being looked into. What can be done however is help = explain what makes John Cook's airplane different. Like other ProJets, it began = as a piston IVP kit. It was modified using a Turbine Solutions (Chris = Skoppe) designed Lancair Turbine retrofit kit. Some major differences with this = kit are the shape of the 35 gal belly tank, a different fuel system = including an air / fuel separator. It's powered with a Diemech / Walter 601-D = engine. It utilizes a Turbine Solution's designed and supplied pressurization = unit - which works much like the King Air Flowpac although it looks very = different - made specifically for the Lancair Propjet. John has the optional = baggage area fuel tank (that I believe is 20 gals). I am told that John flies = with conservative power settings with his ITT in the low - mid 600's. I've = never had the pleasure of flying with John but he does appear to be getting exceptional range for a Turbine - at least from what we've seen on Flightaware. This is a job for an Aerospace Engineer. =20 Hope this helps. =20 Joe =20 -----Original Message----- From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Douglas Kay Sent: Sunday, August 13, 2006 3:33 PM To: Lancair Mailing List Subject: [LML] Re: 4 pt speeds=20 =20 Ok, why is this... according to Lancair,, the D won't pressurize the = plane. Is anything that they told me true? Why would they lie about this stuff anyway? Joe B,, your not a liar are you? What makes this plane faster? D. reddog wrote: In my last post I forgot to mentioned that the 290 knts was the fastest time for the e engine on www.flightaware.com = Most of the times they were around 260 knts to 270 knts I could also = help by divulging the tail numbers John Cooks - N213JC is faster by as much = as 50 knts / others are N420M / N9xW / 750LC take a look = for yourself and see the difference=20 =20 Bill Maddox=20 =20 =20 _____ =20 Do you Yahoo!? Next-gen email? Have it all with the all-new Yahoo! Mail Beta. ------=_NextPart_000_0019_01C6BF0B.202C56C0 Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable

I don’t think anyone can = answer this question at the moment although I understand it’s being looked = into.  What can be done however is help explain what makes John Cook’s = airplane different.  Like other ProJets, it began as a piston IVP kit.  It was modified = using a Turbine Solutions (Chris Skoppe) designed Lancair Turbine retrofit = kit.  Some major differences with this kit are the shape of the 35 gal belly tank, = a different fuel system including an air / fuel separator. =  It’s powered with a Diemech / Walter 601-D engine.  It utilizes a Turbine Solution’s designed and supplied pressurization unit – which = works much like the King Air Flowpac although it looks very different - made = specifically for the Lancair Propjet.  John has the optional baggage area fuel = tank (that I believe is 20 gals).  I am told that John flies with = conservative power settings with his ITT in the low - mid 600’s.  = I’ve never had the pleasure of flying with John but he does appear to be = getting exceptional range for a Turbine – at least from what we’ve seen on = Flightaware.  This is a job for an Aerospace Engineer.

 

Hope this helps.

 

Joe

 

-----Original = Message-----
From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Douglas Kay
Sent: Sunday, August 13, 2006 3:33 = PM
To: Lancair Mailing List
Subject: [LML] Re: 4 pt = speeds

 

Ok, why is this... according to Lancair,, the = D won't pressurize the plane.

Is anything that they told me = true?

Why would they lie about this stuff = anyway?

Joe B,, your not a liar are = you?

What makes this plane = faster?

D.

reddog = <reddog@bentonrea.com<= /i>> = wrote:

In my last post I forgot to mentioned  that the 290 knts was the fastest  time for the e = engine on www.flightaware.com =  Most of the times they were around 260 knts to 270 knts   I could also = help by divulging the tail numbers John Cooks  - N213JC is faster by as = much as 50 knts       /      = others are N420M   /  N9xW   / 750LC  take = a look for yourself and see the difference

    &nbs= p;            = ;            =             &= nbsp;           &n= bsp;           &nb= sp;               &= nbsp;           &n= bsp;           &nb= sp;           &nbs= p;            = ;            =             &= nbsp;           &n= bsp;           &nb= sp;  Bill Maddox

 

 

Do you Yahoo!?
Next-gen email? Have it all with the all-new Yahoo! Mail Beta.

------=_NextPart_000_0019_01C6BF0B.202C56C0--