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Forum: Tech Log

10th Dec 2006, 16:28

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

Wow! thanks for your time and trouble. i think...

Wow!
thanks for your time and trouble. i think i can see what they are saying even if i cant see how they are saying it.
guess i am going to have to ask them direct how they get their numbers? ...

Forum: Tech Log

10th Dec 2006, 09:01

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

OK Thanks, By the way, dont you sleep?? Some...

OK Thanks, By the way, dont you sleep??
Some background data. All from the same source
An aircraft on wheels weighing
Aircraft main wheels are at 12.871M
Nose wheel 4.089M
Main jack points at...

Forum: Tech Log

9th Dec 2006, 21:10

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

OK thanks it sure helps when I understand why...

OK thanks it sure helps when I understand why something works.

theres an on wheels weighing formula that involves the sine of the pitch angle to get to the H-arm. Hows that work then??

cheers...

Forum: Tech Log

9th Dec 2006, 17:09

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

Thanks Is there a decent resource out there...

Thanks

Is there a decent resource out there that lists all these different methods so I could evaluate the most appropriate method?

Cheers
Nobby

Forum: Tech Log

9th Dec 2006, 09:39

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

If I said a certain European aircraft consortiums...

If I said a certain European aircraft consortiums STC manufacturer aircraft weighing reports. Would that be enough for you without me facing libel charges ?
although they call it "calcul du...

Forum: Tech Log

8th Dec 2006, 19:48

Replies: 14

Balance computation in %MAC

Views: 2,097

Posted By nobbyknownowt

Balance computation in %MAC

:uhoh:
ARRRGGGGHHHHH!!!!
in the calculation a - (b*RA)/W where
a= distance of fulcrum (mainwheel jacking point)
b= distance difference between jacking points (nose and mainwheel)
RA = weight...

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