X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 1 [X] Return-Path: Sender: To: lml Date: Sat, 30 Dec 2006 22:05:42 -0500 Message-ID: X-Original-Return-Path: Received: from imo-m27.mx.aol.com ([64.12.137.8] verified) by logan.com (CommuniGate Pro SMTP 5.1.4) with ESMTP id 1726275 for lml@lancaironline.net; Sat, 30 Dec 2006 17:13:23 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.12.137.8; envelope-from=Sky2high@aol.com Received: from Sky2high@aol.com by imo-m27.mx.aol.com (mail_out_v38_r7.6.) id q.cac.76329dc (32915) for ; Sat, 30 Dec 2006 17:12:31 -0500 (EST) From: Sky2high@aol.com X-Original-Message-ID: X-Original-Date: Sat, 30 Dec 2006 17:12:29 EST Subject: Re: [LML] LNC2 electrical schematic X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="-----------------------------1167516749" X-Mailer: 9.0 Security Edition for Windows sub 5358 X-Spam-Flag: NO -------------------------------1167516749 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit In a message dated 12/30/2006 1:24:11 P.M. Central Standard Time, kneadedpleasures@sbcglobal.net writes: No particular hurry to this but I know that I could learn important things from you in seeing an electrical diagram/schematic of your LNC2. Have you ever developed one that you could share in .jpg or .pdf? Although it would be difficult and expensive to completely rewire our aircraft, perhaps adding a simplified essential bus would not be too involved. Greg, My system was defined in the 1994 time frame using Aero Electric's scheme for the essential bus logic. I don't have a diagram and after looking at my original general layout I realized how much of it has changed. Subtracting a Loran, GPS 155, 50 pin GPS-AP switch, Terra comm, Terra Nav, Terra ADF, LASAR ignition and adding an AOA device, 2 electric operated trims, Garmin 430, leg landing light, light wig-wag device, defrost fan, GPSS, air traffic detector, Light Speed Electronic ignition and backup battery, etc. have certainly left me with no usable diagrams at all. However, using 20 pullable CBs, a 20 element fuse block, some inline fuses and a very large Fast-on grounding block certainly helped in allowing the electrical system adapt to the changes. The essential bus is best described in the Aero-Electric documentation - well worth the money. _http://www.aeroelectric.com/Catalog/pub/pub.html_ (http://www.aeroelectric.com/Catalog/pub/pub.html) Scott Krueger AKA Grayhawk Lancair N92EX IO320 SB 89/96 Aurora, IL (KARR) A man has got to know his limitations. -------------------------------1167516749 Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable
In a message dated 12/30/2006 1:24:11 P.M. Central Standard Time,=20 kneadedpleasures@sbcglobal.net writes:
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>No=20 particular hurry to this but I know that I could learn important=20 things from you in seeing an electrical diagram/schematic of your=20 LNC2.  Have you ever developed one that you could share in .jpg=20= or=20 .pdf?  Although it would be difficult and expensive to completely rew= ire=20 our aircraft, perhaps adding a simplified essential bus would not be=20= too=20 involved.
Greg,
 
 My system was defined in the 1994 time frame using Aero Electric'= s=20 scheme for the essential bus logic.  I don't have a diagram and after=20 looking at my original general layout I realized how much of it has=20 changed.  Subtracting a Loran, GPS 155, 50 pin GPS-AP switch, Terra com= m,=20 Terra Nav, Terra ADF, LASAR ignition and adding an AOA device, 2=20 electric operated trims, Garmin 430, leg landing light, light wig-wag device= ,=20 defrost fan, GPSS, air traffic detector, Light Speed Electronic ignition and= =20 backup battery, etc. have certainly left me with no usable diagrams at=20 all. 
 
However, using 20 pullable CBs, a 20 element fuse block, some inli= ne=20 fuses and a very large Fast-on grounding block certainly helped in allo= wing=20 the electrical system adapt to the changes. 
 
The essential bus is best described in the Aero-Electric documentation=20= -=20 well worth the money.
 
http://www.aeroele= ctric.com/Catalog/pub/pub.html =20
 
Scott Krueger=20 AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)

A m= an=20 has got to know his limitations.
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