Max fuel imbalance demonstration
G'day flight testers,
Just came up in the type rating as a discussion.
AFM shows max fuel imbalance 360 kg (some 800 lbs).
The question is: What if a leak empties one of my wings completely. Low wing aircraft engines underslung like E190/A320/737.
FAR 25.343 hints in the direction. But I was not able to find more specific demonstration requirements. Any of you able to enlighten me on how this is tested?
I would expect the aircraft to be flyable for a landing with maybe major trim changes on the aileron and rudder but still manageable for a landing.
Thanks for enlightenment