X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [207.46.163.208] (HELO na01-bl2-obe.outbound.protection.outlook.com) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTPS id 6691918 for lml@lancaironline.net; Fri, 17 Jan 2014 17:16:28 -0500 Received-SPF: pass receiver=logan.com; client-ip=207.46.163.208; envelope-from=rpastusek@htii.com Received: from CO2PR07MB556.namprd07.prod.outlook.com (10.141.199.152) by CO2PR07MB554.namprd07.prod.outlook.com (10.141.199.150) with Microsoft SMTP Server (TLS) id 15.0.851.15; Fri, 17 Jan 2014 22:15:44 +0000 Received: from CO2PR07MB556.namprd07.prod.outlook.com ([10.141.199.152]) by CO2PR07MB556.namprd07.prod.outlook.com ([10.141.199.152]) with mapi id 15.00.0851.011; Fri, 17 Jan 2014 22:15:44 +0000 From: Robert R Pastusek To: Lancair Mailing List Subject: RE: [LML] Re: JACK CUP POINT END Thread-Topic: [LML] Re: JACK CUP POINT END Thread-Index: AQHPE53Yb0N+1CVUuE2qmV/UObuNc5qJcv5g Date: Fri, 17 Jan 2014 22:15:43 +0000 Message-ID: References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: x-originating-ip: [108.28.164.93] x-forefront-prvs: 0094E3478A x-forefront-antispam-report: SFV:NSPM;SFS:(10019001)(679001)(779001)(689001)(24454002)(199002)(189002)(377454003)(129404003)(31966008)(93136001)(92566001)(74502001)(93516002)(74662001)(47446002)(56776001)(15202345003)(79102001)(81542001)(77982001)(59766001)(16236675002)(81342001)(76786001)(76796001)(76576001)(66066001)(65816001)(80022001)(54316002)(74316001)(74876001)(74706001)(63696002)(69226001)(74366001)(49866001)(47736001)(85852003)(19300405004)(51856001)(81686001)(53806001)(47976001)(83072002)(50986001)(4396001)(33646001)(46102001)(87266001)(87936001)(15975445006)(80976001)(2656002)(56816005)(81816001)(90146001)(19580395003)(19580405001)(83322001)(54356001)(76482001)(85306002)(24736002)(217873001);DIR:OUT;SFP:1102;SCL:1;SRVR:CO2PR07MB554;H:CO2PR07MB556.namprd07.prod.outlook.com;CLIP:108.28.164.93;FPR:;RD:InfoNoRecords;A:1;MX:1;LANG:en; Content-Type: multipart/alternative; boundary="_000_e4e0f43f39e4453c81e2e468b102ded2CO2PR07MB556namprd07pro_" MIME-Version: 1.0 X-OriginatorOrg: htii.com --_000_e4e0f43f39e4453c81e2e468b102ded2CO2PR07MB556namprd07pro_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable George, If the IV/IV-P was built according to the plans, the two fuselage jack poin= ts should be immediately forward of the main wing spar box and about 20" ei= ther side of the fore/aft centerline, on the bottom of the fuselage. The ja= cking "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 appea= r as two round 3/8" holes, and a 3/8" fine thread bolt should screw into th= em. 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 we= lded 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 airpla= ne thanks peter --_000_e4e0f43f39e4453c81e2e468b102ded2CO2PR07MB556namprd07pro_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

George,

If the IV/IV-P was built according to the plans, th= e 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 v= ertical steel tubes that are bolted to the front of the spar box. These sho= uld 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 sc= rew into them. The jacking cups themselves consist of steel “cupsR= 21; 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 s= crews into the fuselage.

Hope this helps.

BOB<= o:p>

Where are these points located on the fuselage?<= /span>

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

HI T= HERE

does anyone have a pair of jack point cups.

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

thanks

peter

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