Where can I find a table for maximum load factor (g forces) that an E190(AR) has been certificed for (or tested for) at various flap / flight configurations?

Hello,

I am writing a coursework regarding a plane incident and one of the components involves comparing load factor experienced by the flight (i have that calculated) against load factor g forces that the aircraft has been certified for at various flap settings and configurations.

Does anyone have a source or the best way to find a source?

Many thanks