X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 18 Jan 2014 19:30:24 -0500 Message-ID: X-Original-Return-Path: Received: from nm11-vm10.access.bullet.mail.bf1.yahoo.com ([216.109.114.233] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTPS id 6693106 for lml@lancaironline.net; Sat, 18 Jan 2014 18:23:54 -0500 Received-SPF: none receiver=logan.com; client-ip=216.109.114.233; envelope-from=sdfields68@att.net Received: from [66.196.81.155] by nm11.access.bullet.mail.bf1.yahoo.com with NNFMP; 18 Jan 2014 23:23:19 -0000 Received: from [98.138.104.100] by tm1.access.bullet.mail.bf1.yahoo.com with NNFMP; 18 Jan 2014 23:23:19 -0000 Received: from [127.0.0.1] by smtp120.sbc.mail.ne1.yahoo.com with NNFMP; 18 Jan 2014 23:23:19 -0000 X-Yahoo-Newman-Id: 115966.12697.bm@smtp120.sbc.mail.ne1.yahoo.com X-Yahoo-Newman-Property: ymail-3 X-YMail-OSG: kZ33a7wVM1kdquV8rS8ViKk2xqkQ6_ZoLnyraMIr06GYlPs d6pNMKgBQe0ieUbJgO1u_mbvnOiQpXXhsmBX2OuDB8Q3XOTxH3clNjx0hXKN FY1jtayDb8Qg8G42aI9_OuNs7JHOiz0ZekCvEaKy0PyBKQn9GN4crTcxSeyz kRyM8alcFjCONGQ.hbwFWxXTXBSWHAW8EbL_WwV2GKnDI57niRrJ1xHHrSgB 4yydquoJi_O_4rhZRTwn8YXG2TGqC98cMLgACig_PJess9Xi7lOpzYb9ecJn 36yq906VCkNbeujt.1XxIBFyzWA9jStFsJoOjtToQmhO77eTY2oo2FaTqKxU jgzV6iGxIO6fzf_gWcWgDOsopTNJ0rm7GMvsl4wwQrunI33.pk1vhsnzBsCh ms4TYBFmukGz61wqgDDG1jXT3Khfq.P0MrkuQMaYyJ8njzgkUrR32jsHfbLZ yTnrfkZPsa90UB9_URhgLuFJ.NOmti4.QJsJwvftzl4CCOd_ibt.z2hEo7Ks el1Q2f95NbvJBaMqVUscfutWMVmz_3_Z6XbRfICyekaFKTuaHCe66Ng09aBc A2tFS9BXyLf263PAYdk_7UeoNp6mxYDmSCK9VTHsxQmsw4AcVESYDsF_yP9Y YY8XgqFyP.hDDOP9ZoNV2Y62RVOskxqS0FkTP80B6pRmK9kNYJmRuyg-- X-Yahoo-SMTP: oOs2YV.swBD88T6A.ZRi5opgiddpIVJ9zKnfW4KnPw-- X-Rocket-Received: from Study (sdfields68@108.232.180.239 with plain [98.138.84.52]) by smtp120.sbc.mail.ne1.yahoo.com with SMTP; 18 Jan 2014 23:23:19 +0000 UTC From: "Stan Fields" X-Original-To: "'Lancair Mailing List'" References: In-Reply-To: Subject: RE: [LML] Re: JACK CUP POINT END X-Original-Date: Sat, 18 Jan 2014 17:23:21 -0600 X-Original-Message-ID: <003d01cf14a4$48f547a0$dadfd6e0$@net> MIME-Version: 1.0 Content-Type: multipart/related; boundary="----=_NextPart_000_003E_01CF1471.FE5AD7A0" X-Mailer: Microsoft Office Outlook 12.0 Thread-Index: Ac8UgxfSo3QH9vT8RcW5f+kcPEUicAAIBYtg Content-Language: en-us This is a multi-part message in MIME format. ------=_NextPart_000_003E_01CF1471.FE5AD7A0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_003F_01CF1471.FE5AD7A0" ------=_NextPart_001_003F_01CF1471.FE5AD7A0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit Thanks Jay that is good to know. I built in jack points in my Legacy and had planned to use Jack point cups used on the Mooney. These are offered by Bogert Aviation for $80/Pair. http://bogertaviation.com/index.php?page=shop.product_details&product_id=27& category_id=25&flypage=garden_flypage.tpl&pop=0&option=com_virtuemart&Itemid =23 Stan Fields From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Jay Phillips Sent: Saturday, January 18, 2014 1:26 PM To: lml@lancaironline.net Subject: [LML] Re: JACK CUP POINT END Lancair sells these. I bought a pair a year or two ago. If memory serves there were $50-ish each. Jay Phillips From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Robert R Pastusek Sent: Friday, January 17, 2014 3:16 PM To: Lancair Mailing List Subject: [LML] Re: JACK CUP POINT END George, If the IV/IV-P was built according to the plans, the two fuselage jack points should be immediately forward of the main wing spar box and about 20" either side of the fore/aft centerline, on the bottom of the fuselage. The jacking "cups" thread into vertical steel tubes that are bolted to the front of the spar box. These should be visible under the front edge of the pilot/copilot seats. If you're looking from under the airplane, they should appear as two round 3/8" holes, and a 3/8" fine thread bolt should screw into them. The jacking cups themselves consist of steel "cups" that will fit over the top of a jack head (about 1" in diameter) with a threaded 3/8" shaft welded to the back side.this part screws into the fuselage. Hope this helps. BOB Where are these points located on the fuselage? On Jan 16, 2014, at 9:12 AM, PETER WILLIAMS wrote: HI THERE does anyone have a pair of jack point cups. this is screwed into the bottom of the fuselage when you jack up the airplane thanks peter ------=_NextPart_001_003F_01CF1471.FE5AD7A0 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Thanks Jay that is good to know. I built in jack points in my Legacy = and had planned to use Jack point cups used on the Mooney. These are = offered by Bogert Aviation for $80/Pair.

 

http://bogertaviation.com/index.php?page=3Dshop.product_details&pr= oduct_id=3D27&category_id=3D25&flypage=3Dgarden_flypage.tpl&p= op=3D0&option=3Dcom_virtuemart&Itemid=3D23

<= p class=3DMsoNormal> 

Stan Fields

 

From:= = Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of = Jay Phillips
Sent: Saturday, January 18, 2014 1:26 = PM
To: lml@lancaironline.net
Subject: [LML] Re: JACK = CUP POINT END

 

Lancair sells these. I bought a pair a year or two ago. If memory = serves there were $50-ish each.

 

Jay Phillips

 

From:= = Lancair Mailing List [mailto:lml@lancaironline.net] = On Behalf Of Robert R Pastusek
Sent: Friday, January = 17, 2014 3:16 PM
To: Lancair Mailing List
Subject: = [LML] Re: JACK CUP POINT END

 

George,

If the IV/IV-P was built according to the plans, the two fuselage = jack points should be immediately forward of the main wing spar box and = about 20” either side of the fore/aft centerline, on the bottom of = the fuselage. The jacking “cups” thread into vertical steel = tubes that are bolted to the front of the spar box. These should be = visible under the front edge of the pilot/copilot seats. If you’re = looking from under the airplane, they should appear as two round = 3/8” holes, and a 3/8” fine thread bolt should screw into = them. The jacking cups themselves consist of steel “cups” = that will fit over the top of a jack head (about 1” in diameter) = with a threaded 3/8” shaft welded to the back side…this part = screws into the fuselage.

 

Hope this helps.


BOB<= /span>

 

Where are these points located on the = fuselage?

 

 

On = Jan 16, 2014, at 9:12 AM, PETER WILLIAMS <peterpawaviation@hotmail.com= > wrote:

 

HI = THERE

does anyone have a pair of jack point cups.

this is = screwed into the bottom of the fuselage when you jack up the = airplane

thanks

peter

 

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