View Full Version : A320 lift weight C of G

Black Pudding
5th Jun 2015, 15:01
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

6th Jun 2015, 07:57
Am I wrong ?Yes

A330 - Longitudinal Stability [Archive] - PPRuNe Forums (http://www.pprune.org/archive/index.php/t-377199.html)




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