A320 lift weight C of G
 

A few years ago, I am sure I read that the lift position was slightly ahead of the C of G on Airbus meaning the tail plane was having to create a lift force and not a down force to fly level, adding to the total lift and thus saving fuel ? Been trying to find this info. Am I wrong ? Any thoughts

Yes

A330 - Longitudinal Stability [Archive] - PPRuNe Forums

http://arrow.utias.utoronto.ca/~liu/...on_3_Paper.pdf

http://ac.els-cdn.com/S1877705811027...dd6d09dfb0e148

http://repository.tudelft.nl/assets/...ten_Jansen.pdf

Should keep you off the streets for a while. :)