X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Sun, 13 Aug 2006 15:28:56 -0400 Message-ID: X-Original-Return-Path: Received: from [65.175.65.251] (HELO mta1.webminders.com) by logan.com (CommuniGate Pro SMTP 5.1c.2) with ESMTPS id 1319455 for lml@lancaironline.net; Sat, 12 Aug 2006 01:05:47 -0400 Received-SPF: none receiver=logan.com; client-ip=65.175.65.251; envelope-from=jskiba@icosa.net Received: from 48.sub-70-208-88.myvzw.com ([70.208.88.48] helo=dimension4550) by mta1.webminders.com with esmtpa (Exim 4.60) (envelope-from ) id 1GBlgA-0000oG-I1 for lml@lancaironline.net; Sat, 12 Aug 2006 00:05:01 -0500 From: "Jeffrey W. Skiba" X-Original-To: "'Lancair Mailing List'" Subject: Legacy Landing Gear Hydraulics X-Original-Date: Sat, 12 Aug 2006 00:05:04 -0500 X-Original-Message-ID: <00a801c6bdcc$e1506c00$3058d046@dimension4550> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_00A9_01C6BDA2.F87A6400" X-Mailer: Microsoft Office Outlook 11 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 Thread-Index: Aca9pTHWrn227K03Tq+LRqD+AOOlRQAJ3xlg In-Reply-To: X-Headers-Begin: 1GBlgA-0000oG-I1 X-Authenticated-As: X-Headers-End: 1GBlgA-0000oG-I1 This is a multi-part message in MIME format. ------=_NextPart_000_00A9_01C6BDA2.F87A6400 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit The legacy has a system at aerocraft http://www.aerocraftparts.com/ItemForm.aspx?item=800-0010 lists at $2,310.00 FYI _____ From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Bryan Burr Sent: Friday, August 11, 2006 7:21 PM To: Lancair Mailing List Subject: [LML] Legacy Landing Gear Hydraulics Jan Fronk of Highridge Design, Provo, Utah is an engineer who has developed a beautiful hydraulic system that controls the extension/retraction of landing gears and gear doors for the Stewart S-51 Mustang Replica. Currently there are 15 of his kits being installed. They are of the highest quality. His system would integrate downstream from existing hydraulic pumps. I was talking with him about the possibility of adapting them to work with the Legacy and Lancair IV aircraft and he is most interested. He asked me to make a posting to the LML and see if there is any interest. His Hydraulic Sequencing Control Unit would provide the following: 1. Electronic computer controlled manifold valves that control landing gear extension/retraction and door sequencing. 2. Development of landing gear inner doors that are sequenced and controlled by the same electronic manifold valve 3. Electronic controlled spool cartridge valves for hydraulic fluid direction control 4. All hydraulic actuators 5. All mounting plates, wiring harness, and hardware 6. Detailed installation instructions 7. Circuit protected logic boards including static electricity protection 8. Processor Code is Watch Dog protected This is the system for the S-51 Mustang. If there is interest for the Legacy / IV aircraft then he would begin an adaptation program. Currently the price for the S-51 is $3875.00. It seems there has been much discussion on the LML about hydraulic problems encountered in the Legacy systems. Perhaps solutions could be incorporated into the retrofit program of Jan's system. Your comments and replies are appreciated. Bryan J. Burr Super ES N132BB ------=_NextPart_000_00A9_01C6BDA2.F87A6400 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

The legacy has a system at = aerocraft

http= ://www.aerocraftparts.com/ItemForm.aspx?item=3D800-0010

lists at $2,310.00 

FYI

From: = Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Bryan Burr
Sent: Friday, August 11, = 2006 7:21 PM
To: Lancair Mailing = List
Subject: [LML] Legacy = Landing Gear Hydraulics

 

Jan Fronk of Highridge Design, Provo, Utah is an engineer who has developed a beautiful hydraulic system that = controls the extension/retraction of landing gears and gear doors for the Stewart = S-51 Mustang Replica.  Currently there are 15 of his kits being installed.  They are of the highest quality.  His system would integrate downstream from existing hydraulic = pumps.

 

I was talking with him about the possibility of = adapting them to work with the Legacy and Lancair IV aircraft and he is most interested.  He asked me to make a posting to the LML and see if = there is any interest.

 

His Hydraulic Sequencing Control Unit would provide = the following:

  1. Electronic computer = controlled manifold valves that control landing gear extension/retraction and = door sequencing.
  2. Development of landing = gear inner doors that are sequenced and controlled by the same = electronic manifold valve
  3. Electronic controlled = spool cartridge valves for hydraulic fluid direction = control
  4. All hydraulic = actuators
  5. All mounting plates, = wiring harness, and hardware
  6. Detailed installation instructions
  7. Circuit protected = logic boards including static electricity = protection
  8. Processor Code is = Watch Dog protected

 

This is the system for the S-51 Mustang.  If = there is interest for the Legacy / IV aircraft then he would begin an adaptation program.  Currently the price for the S-51 is = $3875.00.

 

It seems there has been much discussion on the LML = about hydraulic problems encountered in the Legacy systems.  Perhaps = solutions could be incorporated into the retrofit program of Jan’s = system.

 

Your comments and replies are = appreciated.

 

Bryan J. Burr

Super ES

N132BB

 

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