Mailing List lml@lancaironline.net Message #44468
From: Lorn H Olsen <lorn@dynacomm.ws>
Sender: <marv@lancaironline.net>
Subject: Re: spry shocks
Date: Wed, 17 Oct 2007 21:22:08 -0400
To: <lml@lancaironline.net>
My empty (w/oil) wheel weights are:

               Main                     Moment Arm
   Nose    Left    Right   Total     Prop    Firewall
    388     413     383    1,184     58.6  or  22.3

I know that the left wheel is heavier but I do not know why. It has to be just paint.

I calculated the following with a spreadsheet by using the moment arms. My nose and main gear arms are 29 and 73 inches respectively.
My gross (calculated) weights are:

               Main                     Moment Arm
   Nose    Left    Right   Total     Prop    Firewall
    313   793.5    793.5   1,900     65.8  or  29.5

I am attaching an Excel spreadsheet to help others calculate the gross weight distribution on the wheels.

I didn't realize how much lighter the nose gear load got as the plane is loaded?

Lorn

From: Sky2high@aol.com
Date: October 13, 2007 6:43:08 PM GMT-04:00

In a message dated 10/12/2007 7:00:32 P.M. Central Daylight Time, n103md@yahoo.com writes:
PS Hint: empty, each main should statically be supporting
about 430-450 lbs, depending.

Grayhawk: shouldn't that be 330-350 lbs per wheel empty?
My empty weight is 1030 lbs (Lancair 235 / O-320).
.
.
--
Lorn H. 'Feathers' Olsen, MAA, DynaComm, Corp.
248-345-0500, mailto:lorn@dynacomm.ws
LNC2, FB90/92, O-320-D1F, 1,300 hrs, N31161, Y47, SE Michigan

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