Maximum civil aircraft pitch angle during normal operation
I am interested in knowing what sort of maximum pitch angles occur in the current (large civil) fleet during normal operation at take-off? My guess is that a light 757 operating out of somewhere like John Wayne would be near the maximum seen in practice but does anyone know what this is?
My interest stems from looking at low noise operations of future aircraft so am more interested in limits imposed by airlines for passenger comfort than limits imposed by aircraft capability. Any references to published documentation would be great.
Thanks.