Does anyone know (roughly) how much aileron trim would be required to maintain level flight in the 737 with maximum allowed fuel imbalance of 1000 lbs (453 kg)?
I found
this publication by Boeing quoting a figure of 0.25 to 0.5 unit for the 747 flying with a maximum lateral imbalance - would it be safe to assume similar figures for the 737?
Just curious.
