X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 18 Jan 2014 14:25:37 -0500 Message-ID: X-Original-Return-Path: Received: from p3plsmtpa07-02.prod.phx3.secureserver.net ([173.201.192.231] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTP id 6691967 for lml@lancaironline.net; Fri, 17 Jan 2014 17:59:11 -0500 Received-SPF: none receiver=logan.com; client-ip=173.201.192.231; envelope-from=jayph@fastairplane.net Received: from shuriken ([69.92.48.82]) by p3plsmtpa07-02.prod.phx3.secureserver.net with id FAyc1n00V1mPo4M01Ayc3b; Fri, 17 Jan 2014 15:58:37 -0700 From: "Jay Phillips" X-Original-To: "'Lancair Mailing List'" References: In-Reply-To: Subject: RE: [LML] Re: JACK CUP POINT END X-Original-Date: Fri, 17 Jan 2014 15:58:34 -0700 X-Original-Message-ID: <008f01cf13d7$a69f5530$f3ddff90$@fastairplane.net> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0090_01CF139C.FA407D30" X-Mailer: Microsoft Outlook 14.0 Thread-Index: AQIe2tpfJTI1EaFXjKWDOg/ldMnzh5np+UeA Content-Language: en-us This is a multipart message in MIME format. ------=_NextPart_000_0090_01CF139C.FA407D30 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit 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_000_0090_01CF139C.FA407D30 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

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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