Return-Path: Received: from dub-img-10.compuserve.com ([149.174.206.140]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Thu, 18 Mar 1999 22:11:21 -0500 Received: (from root@localhost) by dub-img-10.compuserve.com (8.8.6/8.8.6/2.18) id WAA19757 for lancair.list@olsusa.com; Thu, 18 Mar 1999 22:13:22 -0500 (EST) Date: Thu, 18 Mar 1999 22:12:49 -0500 From: Rick Argente Subject: Weight & Balance Worksheet Sender: Rick Argente To: "INTERNET:lancair.list@olsusa.com" Message-ID: <199903182213_MC2-6E92-AC74@compuserve.com> Mime-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline X-Mailing-List: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I just recently completed my weight and balance measurements and calculations for my Lancair 360. I used an Excel file which contains a couple of spreadsheets to simplify the calculations and Marv was kind enough to upload this file on to his download area. Please feel free to download this file. It also contains a picture of the aircraft showing the various aircraft stations. After I entered my weights and measurements, I simply printed the worksheets at 75% of the original size and included these in my flight manual. I am confident that the calculations are correct but if somebody finds an error, please let me know. Anyway, here is a brief summary of my results: Aircraft Configuration: IO360 / CS Hartzell Prop / Header Tank / In primer only / Stock motor mount Behind Seatback contains: Hydraulic pump, ELT, Gell battery (Gill), Strobe power source, flap motor. Other accesories: Dual adjustable rudder pedals/brakes, King Nav/Com/GS, Xpndr, EPI 800, Intercom, audio panel, inbd gear door hydraulics. Empty Wt: 1178 lbs. at FS 23.64" Dist from Datum Pt to FS 0 = 37.75" Station Distances from Datum Pt (behind spinner): Nose Wheel: 32.40" Header Fue;l: 45.15" Wing Fuel: 74.75" Main Gear: 75.25" Pilot/Pass: 82.96" Baggage: 114.49" I also included a 'comparison' worksheets from various weight and balance data I have compiled from other builders. I was a bit surprise to find variations in the aircraft station measurements especially the distance between the datum pt. and the nose wheel, up to a 5-inch difference compared to what I came up with. Other station measurements and calculated station distances seems to be within reasonable range differences. Lastly, just for kicks, I also took measurements (both weights and distances) with the fuselage NOT leveled and with the fuselage leveled. The difference in the empty FS numbers was approximately 3/4" (Leveled: FS 23.64 / Not Leveled: FS22.90). Rick Argente (won't be long now ;-)