X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 18 Jan 2014 14:43:14 -0500 Message-ID: X-Original-Return-Path: Received: from nk11p08mm-asmtp002.mac.com ([17.158.58.247] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTP id 6692588 for lml@lancaironline.net; Sat, 18 Jan 2014 11:41:37 -0500 Received-SPF: pass receiver=logan.com; client-ip=17.158.58.247; envelope-from=gw5@me.com Received: from [10.180.227.11] (mobile-166-205-064-250.mycingular.net [166.205.64.250]) by nk11p08mm-asmtp002.mac.com (Oracle Communications Messaging Server 7u4-27.08(7.0.4.27.7) 64bit (built Aug 22 2013)) with ESMTPSA id <0MZL00EURVO7R900@nk11p08mm-asmtp002.mac.com> for lml@lancaironline.net; Sat, 18 Jan 2014 16:41:00 +0000 (GMT) X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.11.87,1.0.14,0.0.0000 definitions=2014-01-18_01:2014-01-18,2014-01-18,1970-01-01 signatures=0 X-Proofpoint-Spam-Details: rule=notspam policy=default score=0 spamscore=0 suspectscore=0 phishscore=0 adultscore=0 bulkscore=0 classifier=spam adjust=0 reason=mlx scancount=1 engine=7.0.1-1308280000 definitions=main-1401180114 Subject: Re: [LML] Re: JACK CUP POINT END References: From: George Wehrung Content-type: multipart/alternative; boundary=Apple-Mail-6F0C2A76-7F4A-477D-9D7C-7ED84E8EEDFA X-Mailer: iPhone Mail (11B554a) In-reply-to: X-Original-Message-id: X-Original-Date: Sat, 18 Jan 2014 11:40:54 -0500 X-Original-To: Lancair Mailing List Content-transfer-encoding: 7bit MIME-version: 1.0 (1.0) --Apple-Mail-6F0C2A76-7F4A-477D-9D7C-7ED84E8EEDFA Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Thanks Bob. I think it was also an option for the ES.=20 Sent from my iPhone > On Jan 17, 2014, at 17:15, Robert R Pastusek wrote: >=20 > George, > If the IV/IV-P was built according to the plans, the two fuselage jack poi= nts should be immediately forward of the main wing spar box and about 20=E2=80= =9D either side of the fore/aft centerline, on the bottom of the fuselage. T= he jacking =E2=80=9Ccups=E2=80=9D thread into vertical steel tubes that are b= olted to the front of the spar box. These should be visible under the front e= dge of the pilot/copilot seats. If you=E2=80=99re looking from under the air= plane, they should appear as two round 3/8=E2=80=9D holes, and a 3/8=E2=80=9D= fine thread bolt should screw into them. The jacking cups themselves consis= t of steel =E2=80=9Ccups=E2=80=9D that will fit over the top of a jack head (= about 1=E2=80=9D in diameter) with a threaded 3/8=E2=80=9D shaft welded to t= he back side=E2=80=A6this part screws into the fuselage. > =20 > Hope this helps. >=20 > BOB > =20 > Where are these points located on the fuselage? > =20 > =20 > On Jan 16, 2014, at 9:12 AM, PETER WILLIAMS = wrote: >=20 >=20 > HI THERE >=20 > does anyone have a pair of jack point cups. >=20 > this is screwed into the bottom of the fuselage when you jack up the airpl= ane >=20 > thanks >=20 > peter > =20 --Apple-Mail-6F0C2A76-7F4A-477D-9D7C-7ED84E8EEDFA Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: quoted-printable
Thanks Bob. I think it was also an opt= ion for the ES. 



Sent from my iPhone

On Jan 17, 2014, at 17:15, Robert R Pastusek <rpastusek@htii.com> wrote:

=

George,

If the IV/IV-P was built according to the plans, the t= wo fuselage jack points should be immediately forward of the main wing spar box and about 20=E2=80=9D either side of the fore/aft centerline,= on the bottom of the fuselage. The jacking =E2=80=9Ccups=E2=80=9D thread in= to vertical steel tubes that are bolted to the front of the spar box. These s= hould be visible under the front edge of the pilot/copilot seats. If you=E2=80=99re looking from under the airplane, they should appea= r as two round 3/8=E2=80=9D holes, and a 3/8=E2=80=9D fine thread bolt shoul= d screw into them. The jacking cups themselves consist of steel =E2=80=9Ccup= s=E2=80=9D that will fit over the top of a jack head (about 1=E2=80=9D in di= ameter) with a threaded 3/8=E2=80=9D shaft welded to the back side=E2=80=A6this par= t 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 <peterpawaviation@hotmail.com> wrot= e:



HI THE= RE

does anyone have a pair of jack point cups.

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

thanks

peter

 

= --Apple-Mail-6F0C2A76-7F4A-477D-9D7C-7ED84E8EEDFA--