Mailing List lml@lancaironline.net Message #69003
From: George Wehrung <gw5@me.com>
Sender: <marv@lancaironline.net>
Subject: Re: [LML] Re: JACK CUP POINT END
Date: Sat, 18 Jan 2014 14:43:14 -0500
To: <lml@lancaironline.net>
Thanks Bob. I think it was also an option 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 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 <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

 

Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster