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Procedure for calculating weight and balance



 
 
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  #111  
Old January 8th 07, 04:40 PM posted to rec.aviation.piloting
Mxsmanic
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Default Procedure for calculating weight and balance

Thomas Borchert writes:

If you fly a cruise speed of 150
knots in a Baron, you'd still have different elevator positions
depending on CG location. In fact, the position would change during the
flight with fuel burn. Which would be "neutral"?


The one that aligns the trim tabs with the control surfaces.

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  #112  
Old January 8th 07, 04:42 PM posted to rec.aviation.piloting
Mxsmanic
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Default Procedure for calculating weight and balance

Kev writes:

In this case, you really need to listen to what Thomas and others are
saying. There is no neutral position. There is just a natural
position for a certain flight regime.


The neutral position for trim tabs is the position in which the trim
tabs are aligned with the control surface. The neutral position for
control surfaces is the position in which they are aligned with the
surfaces to which they are attached (wings or stabilizers).

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  #113  
Old January 8th 07, 05:13 PM posted to rec.aviation.piloting
Gig 601XL Builder
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Default Procedure for calculating weight and balance

Mxsmanic wrote:
Kev writes:

In this case, you really need to listen to what Thomas and others are
saying. There is no neutral position. There is just a natural
position for a certain flight regime.


The neutral position for trim tabs is the position in which the trim
tabs are aligned with the control surface. The neutral position for
control surfaces is the position in which they are aligned with the
surfaces to which they are attached (wings or stabilizers).


Ok Anthony, you have perfectly loaded your aircraft so the that it trims out
to what you like to call nuetra or default. What are you going to do once
you have burned off fuel and the CG changes?


  #114  
Old January 8th 07, 05:22 PM posted to rec.aviation.piloting
Newps
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Default Procedure for calculating weight and balance



Kev wrote:
Newps wrote:

MxIdiot is a complete and utter moron and deserves everything he gets.



Careful. Glass houses and all that.



Fire away.





Plus it's fun.



Dude, do more flying. I can think of a lot more fun things, than
constantly bashing one teenage boy on the net :-)


Wind 280@30G45
  #115  
Old January 8th 07, 05:24 PM posted to rec.aviation.piloting
Newps
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Posts: 1,886
Default Procedure for calculating weight and balance



Mxsmanic wrote:



The neutral position for trim tabs is the position in which the trim
tabs are aligned with the control surface. The neutral position for
control surfaces is the position in which they are aligned with the
surfaces to which they are attached (wings or stabilizers).


What's the neutral position of a Cub or Cessna 180?
  #116  
Old January 8th 07, 05:33 PM posted to rec.aviation.piloting
Gig 601XL Builder
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Posts: 2,317
Default Procedure for calculating weight and balance

Kev wrote:
Dude, do more flying. I can think of a lot more fun things, than
constantly bashing one teenage boy on the net :-)


The problem is he isn't a teenager.

http://www.atkielski.com/


  #117  
Old January 8th 07, 11:07 PM posted to rec.aviation.piloting
Mxsmanic
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Posts: 9,169
Default Procedure for calculating weight and balance

Gig 601XL Builder writes:

What are you going to do once
you have burned off fuel and the CG changes?


Adjust the trim. Ideally, I'd be in an aircraft where the fuel load
is already at that ideal neutral point, and so very little adjustment
would be required.

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  #118  
Old January 8th 07, 11:08 PM posted to rec.aviation.piloting
Mxsmanic
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Posts: 9,169
Default Procedure for calculating weight and balance

Newps writes:

What's the neutral position of a Cub or Cessna 180?


I don't know. I've never flown anything that tiny.

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  #119  
Old January 8th 07, 11:23 PM posted to rec.aviation.piloting
Tony
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Posts: 312
Default Procedure for calculating weight and balance

So sad.



On Jan 8, 6:08 pm, Mxsmanic wrote:
Newps writes:
What's the neutral position of a Cub or Cessna 180?I don't know. I've never flown anything that tiny.


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  #120  
Old January 8th 07, 11:24 PM posted to rec.aviation.piloting
Newps
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Posts: 1,886
Default Procedure for calculating weight and balance



Mxsmanic wrote:




Adjust the trim. Ideally, I'd be in an aircraft where the fuel load
is already at that ideal neutral point, and so very little adjustment
would be required.


No such animal.
 




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