Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Fri, 16 Jan 2004 22:23:58 -0500 Message-ID: X-Original-Return-Path: Received: from tomts36-srv.bellnexxia.net ([209.226.175.93] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2935680 for lml@lancaironline.net; Fri, 16 Jan 2004 20:57:12 -0500 Received: from crowe ([67.69.54.127]) by tomts36-srv.bellnexxia.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with SMTP id <20040117015706.XHWE11804.tomts36-srv.bellnexxia.net@crowe> for ; Fri, 16 Jan 2004 20:57:06 -0500 X-Original-Message-ID: <003901c3dc9d$50769230$6721fea9@crowe> From: "Ian Crowe" X-Original-To: "Lancair Mailing List" Subject: LNC2 Airflow perormance boost pump X-Original-Date: Fri, 16 Jan 2004 20:57:50 -0500 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0036_01C3DC73.67529140" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 This is a multi-part message in MIME format. ------=_NextPart_000_0036_01C3DC73.67529140 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable I may have missed the previous mail but I have the Airflow performance = boost pump and in line filter under the LH seat pan. Plenty of room = there. (The RH side has the wing leveller servo) My fuel line runs = forward from the pump/filter assembly to the fuel transducer for the = fuel flow instrument. This is just forward of the main spar, up against = the nose gear tunnel, right in the corner. You cannot get your feet on = it and I have hidden it behind a fibreglass moulding. From there = through a bulkhead fitting to the gascloator which is on the LH side of = the firewall as low as I can get it. Works like a charm. Fuel burn is = accurate to about 1/2gallon in 42. So the transducer is not affected by = its proximity to the pump. Maybe I missed something so the above is meaningless, but anyhow you now = know what I know which is way ahead of Donald Rumsfeld. (With apologies = to Scott Krueger) Regards Ian Crowe LC2 C-FKRO Only in Canada eh! ------=_NextPart_000_0036_01C3DC73.67529140 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
I may have missed the previous mail but = I have the=20 Airflow performance boost pump and in line filter under the LH seat = pan. =20 Plenty of room there.  (The RH side has the wing leveller = servo) =20 My fuel line runs forward from the pump/filter assembly to the fuel = transducer=20 for the fuel flow instrument.  This is just forward of the main = spar, up=20 against the nose gear tunnel, right in the corner.  You cannot get = your=20 feet on it and I have hidden it behind a fibreglass moulding. From = there =20 through a bulkhead fitting to the gascloator which is on the LH side of = the=20 firewall as low as I can get it.  Works like a charm.  Fuel = burn is=20 accurate to about 1/2gallon in 42.  So the transducer is not = affected by=20 its proximity to the pump.
 
Maybe I missed something so the above = is=20 meaningless, but anyhow you now know what I know which is way ahead of = Donald=20 Rumsfeld. (With apologies to Scott Krueger)
 
Regards
 
Ian Crowe
LC2 C-FKRO Only in Canada=20 eh!
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