X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from imr-ma03.mx.aol.com ([64.12.206.41] verified) by logan.com (CommuniGate Pro SMTP 5.3.4) with ESMTP id 4181040 for flyrotary@lancaironline.net; Sat, 27 Mar 2010 16:55:31 -0400 Received-SPF: pass receiver=logan.com; client-ip=64.12.206.41; envelope-from=Bktrub@aol.com Received: from imo-ma04.mx.aol.com (imo-ma04.mx.aol.com [64.12.78.139]) by imr-ma03.mx.aol.com (8.14.1/8.14.1) with ESMTP id o2RKsoDL005795 for ; Sat, 27 Mar 2010 16:54:50 -0400 Received: from Bktrub@aol.com by imo-ma04.mx.aol.com (mail_out_v42.9.) id q.bc5.6860b194 (43953) for ; Sat, 27 Mar 2010 16:54:46 -0400 (EDT) Received: from smtprly-me02.mx.aol.com (smtprly-me02.mx.aol.com [64.12.95.103]) by cia-dd01.mx.aol.com (v127_r1.2) with ESMTP id MAILCIADD012-b2b84bae7090ed; Sat, 27 Mar 2010 16:54:45 -0400 Received: from webmail-d043 (webmail-d043.sim.aol.com [205.188.167.99]) by smtprly-me02.mx.aol.com (v127_r1.2) with ESMTP id MAILSMTPRLYME022-b2b84bae7090ed; Sat, 27 Mar 2010 16:54:40 -0400 References: To: flyrotary@lancaironline.net Subject: Re: [FlyRotary] Re: Turbo Planning and p-port planning (Long) Date: Sat, 27 Mar 2010 16:54:40 -0400 X-AOL-IP: 208.46.237.130 In-Reply-To: X-MB-Message-Source: WebUI MIME-Version: 1.0 From: bktrub@aol.com X-MB-Message-Type: User Content-Type: multipart/alternative; boundary="--------MB_8CC9C06DACE658A_E80_19342_webmail-d043.sysops.aol.com" X-Mailer: AOL Webmail 31226-STANDARD Received: from 208.46.237.130 by webmail-d043.sysops.aol.com (205.188.167.99) with HTTP (WebMailUI); Sat, 27 Mar 2010 16:54:40 -0400 Message-Id: <8CC9C06DAC01D44-E80-DDFB@webmail-d043.sysops.aol.com> X-Spam-Flag:NO X-AOL-SENDER: Bktrub@aol.com ----------MB_8CC9C06DACE658A_E80_19342_webmail-d043.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset="utf-8" I'd be happy with an N/A all aluminum 2 rotor p-port. Forget the turbo co= mpound for now.=20 Brian Trubee -----Original Message----- From: Al Gietzen To: Rotary motors in aircraft Sent: Sat, Mar 27, 2010 12:52 pm Subject: [FlyRotary] Re: Turbo Planning and p-port planning (Long) =20 To start with, I would like to place an order for the 164 pound, over 200H= P engine please.=20 Mike =20 =20 No problem =E2=80=93 all aluminum, 2-rotor, P-port, turbo-compound. 250HP= at 7000 rpm. How much would you like to pay? =20 Al =3D ----------MB_8CC9C06DACE658A_E80_19342_webmail-d043.sysops.aol.com Content-Type: multipart/related; boundary="--------MB_8CC9C06DACE658A_E80_19343_webmail-d043.sysops.aol.com" ----------MB_8CC9C06DACE658A_E80_19343_webmail-d043.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset="utf-8"
I'd be happy with an N/A  all aluminum 2 rotor p-port. Forg= et the turbo compound for now.
 
Brian Trubee



-----Original Message-----
From: Al Gietzen <ALVentures@cox.net>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Sat, Mar 27, 2010 12:52 pm
Subject: [FlyRotary] Re: Turbo Planning and p-port planning (Long)

 
To start with, I would like to place an order for the 16= 4 pound, over 200HP engine please. 3D"Smile<= /div>
 Mike  
 
No problem =E2= =80=93 all aluminum, 2-rotor, P-port, turbo-compound.  250HP at 7000= rpm.  How much would you like to pay?
 
Al
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