I read here: http://forums.corral.net/forums/11231716-post10.html, that someone went from 57% front down to 53% by moving the engine back. I'm skeptical. I moved our crossmember forward 5/8", and we are at 59%.
Weight:
1692# 58.75% front
1188# 41.25% rear
2880# total
101.125" wheel base
101.125"x58.75%=59.41"
101.125"-59.41"=41.715"
This puts the center of gravity 41.715" behind the front wheels.
If I use 600# for the weight of the motor and trans, and move it back 1", I get:
ΔCG=(weight shifted x distance shifted)/total weight
(600#x1")/2880#=.208"
41.715"+.208"=41.923"
101.125"-41.923"=59.202"
59.202"/101.125"=58.54%
Conclusion:
Moving a 5.0L/T-5 back 1" only shifts the weight balance by 1/4%. Anyone see a problem with my numbers?
Ref:
http://www.faa.gov/regulations_policies/handbooks_manuals/aircraft/media/faa-h-8083-1a.pdf
Weight:
1692# 58.75% front
1188# 41.25% rear
2880# total
101.125" wheel base
101.125"x58.75%=59.41"
101.125"-59.41"=41.715"
This puts the center of gravity 41.715" behind the front wheels.
If I use 600# for the weight of the motor and trans, and move it back 1", I get:
ΔCG=(weight shifted x distance shifted)/total weight
(600#x1")/2880#=.208"
41.715"+.208"=41.923"
101.125"-41.923"=59.202"
59.202"/101.125"=58.54%
Conclusion:
Moving a 5.0L/T-5 back 1" only shifts the weight balance by 1/4%. Anyone see a problem with my numbers?
Ref:
http://www.faa.gov/regulations_policies/handbooks_manuals/aircraft/media/faa-h-8083-1a.pdf