"Tarver Engineering" wrote...

Airbus hadn't programmed their A-320 to do what the operator commanded.

Hmmm... I suspect that when the pilot added go-around power, he commanded
the
airplane to provide maximum lift/minimum sink while the engines spooled up.

In what wy do you believe that stalling the wing is within the flight
envelope?

In what way do you believe stalling the wing had anything to do with the late
go-around attempt?

What flight envelope?