I am in full agreement with Larry especially in the reasoning that it has to be 
considered from the start. N357CJ was built from the start with an eye on 
weight and location of that mass. I know places that I could have improved and 
actually saved some weight but over all it turned out pretty dang good. My 
battery is in the front and no extra weight had to be added to get weight and 
balance in the foreword part of the range. The Dr. Dean plane that I am working 
on now is another story. While it has some very nice looking parts they are 
incredibly heavy, like the horizontal stab and elevator assembly, fully 
completed when I got it. It weighed just over 21# which is 2 ?times what N357CJ 
has in the whole tail assembly. Consider that all of that is as far back as it 
can get. I managed to reduce that part alone by nearly 7# but it is still going 
to give me trouble latter. Even with some experience under my belt I still am 
lacking in my planning as I have not fully calculated things out for the Dr. 
Dean plane. Actually just working with gut feelings right now til I get to 
where I can mount the engine and get some real feel for where it is headed. I 
have an over all goal of bring it in at or below 700# empty weight.
?? ?Still the under laying thought with every part that I make and install is 
where it is in relation to the wing and can I do better. Most times the answer 
is yes it can be ?lighter or located differently.
Joe Horton,
1 in the hanger - 1 in the shop



?As builders make changes , lengthen fuselage, heavier 
engines, fuel tank changes, balanced elevators, etc., they must take 
in to account this balancing act. ?The further you get in to the 
project and realize an error, the harder it is to correct.

?Just remember, it's the C of L we need to work around, 
that being basically the C.G. spec's given in the plans.

Larry Flesner 


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