The problem with these things is that everything you do changes the 
CG---------including leaning forward. Somebody needs to invent a sliding 
counter weight. ( just kidding)



----- Original Message ----- 
From: "Colin Rainey" <brokerpilot9...@earthlink.net>
To: <kr...@mylist.net>
Sent: Wednesday, January 04, 2006 7:24 PM
Subject: KR> CG and the KR2S


> Kenny and Bobby
> My initial post was in response to a question posed by a builder in 
> reference to whether or not the CG location and limits were different from 
> the original KR2 and the KR2S.  I had stated that they were not if both 
> aircraft were built to plans. Kenny your plane being flown within 2 inches 
> of the aft limit basically puts the aircraft at the "sane" limit that all 
> who are informed about the KR2 and S agree on.  A quick weight and balance 
> check of the shifting of the CG slightly aft as you take off and begin 
> climb would probably reveal that you are in fact in that last 2 inches 
> during the climb, and so need to take measures to keep the CG forward at 
> all times.  I am loading everything that I can that I have to put in the 
> plane anyway in front of the main spar in some way or another.  The more 
> weight that I can transfer to right at or just ahead of the spar, the 
> harder it will be to move the CG rearward due to the volume already 
> forward. Also, I plan to have a small fuel cell used when
> flying with two, behind the seat so that when flying long distance, and 
> draining the header tank, I can re-fill it with 5 to 6 gallons to maintain 
> a safe CG in descent and landing, while manipulating the CG aft while in 
> cruise. Yes there will be 2 pumps to transfer fuel so that I cannot get 
> caught with an out of CG plane...
>
> New latch in the new gullwing. Back to sanding the nose bowl to shape...
>
>
> Colin Rainey
> First National Mortgage Sources
> Lending Solutions in All 50 States
> brokerpilot9...@earthlink.net
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