X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 22 Apr 2011 13:56:52 -0400 Message-ID: X-Original-Return-Path: Received: from mta31.charter.net ([216.33.127.82] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with ESMTP id 4954221 for lml@lancaironline.net; Fri, 22 Apr 2011 09:13:10 -0400 Received-SPF: pass receiver=logan.com; client-ip=216.33.127.82; envelope-from=toms1@chartermi.net Received: from imp11 ([10.20.200.11]) by mta31.charter.net (InterMail vM.7.09.02.04 201-2219-117-106-20090629) with ESMTP id <20110422131234.ICCW7341.mta31.charter.net@imp11> for ; Fri, 22 Apr 2011 09:12:34 -0400 Received: from beth ([24.231.140.52]) by imp11 with smtp.charter.net id adCa1g00A181idC05dCa9D; Fri, 22 Apr 2011 09:12:34 -0400 X-Authority-Analysis: v=1.1 cv=LG388EjIwmnRE/vJMJE0apjUdCKzeapOUwUcQ6XFns4= c=1 sm=1 a=2YB2Jhyzo0YA:10 a=7Vtkk4Wg9cEA:10 a=6z0E4Jrb22jZ/GE9j9Htdg==:17 a=tgSe97erCtDIEOPZHjIA:9 a=wPNLvfGTeEIA:10 a=6VdOu-3Sdj6X0GiG63kA:9 a=w5ZbtyNSh-QuNwYo0pwA:7 a=6z0E4Jrb22jZ/GE9j9Htdg==:117 X-Original-Message-ID: From: "Tom & Beth Sullivan" X-Original-To: Subject: IVPT A/C & Aft fuselage area questions X-Original-Date: Fri, 22 Apr 2011 08:12:41 -0500 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0059_01CC00C5.0D3E5D50" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5931 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5994 This is a multi-part message in MIME format. ------=_NextPart_000_0059_01CC00C5.0D3E5D50 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable As we're finishing up the A/C condenser mounting, wiring and = plumbing, my part time build helper, an A&P, and I were looking at the = space left in the aft fuselage area, wondering what we have left to fit = in there? I'm thinking ELT and what else? I would like to complete as = much as possible before temporarily installing the top and fitting the = door. =20 The autopilot installation came up and we are wondering if the = autopilots typically used in the IVP are "trim tab" driven (I have Ray = Allen servos on all of my trim tabs), or are there servo's hooked = directly to flight control tubes? Specifically, we are wondering if we = will need to mount some type of servo to the elevator push/pull tube? I've also fabricated mounts and installed the evaporator and fan on = the rear pressure bulkhead (all of my own design) and wondering if = anyone has pictures of this area during different phases of completion? Thanks in advance Tom Sullivan Refocused and making progress!! ------=_NextPart_000_0059_01CC00C5.0D3E5D50 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

As = we're finishing up the=20 A/C condenser mounting, wiring and plumbing, my part time build helper, = an=20 A&P, and I were looking at the space left in the aft=20 fuselage area, wondering what we have left to fit in there? = I'm=20 thinking ELT and what else? I would like to complete as much as = possible=20 before temporarily installing the top and fitting the door. =

The autopilot installation came = up and we=20 are wondering if the autopilots typically used in the IVP are "trim = tab"=20 driven (I have Ray Allen servos on all of my trim tabs), or are there = servo's=20 hooked directly to flight control tubes? Specifically, we are = wondering if=20 we will need to mount some type of servo to the elevator push/pull=20 tube?

I've also fabricated mounts and installed the evaporator and = fan on=20 the rear pressure bulkhead (all of my own design) and wondering if = anyone has=20 pictures of this area during different phases of completion?

Thanks in advance

Tom Sullivan

Refocused and making progress!!

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