Ex Non-pilot aircrew here.
I have experienced compressor stalls on B727 climb outs after which our erstwhile flight engineer would explain this away as being attributed to the fuselage creating a shadow during high angle climb outs. It certainly felt like we launching a rocket at times from some short fields and this was then sometimes followed by a 'boom boom' in quick succession.Indications on the flight deck always found No 2 was the culprit.
But what causes a compressor to stall on a T7? Is it a function of heavy TO weight and high alpha on climb out and if so, would not both engines suffer in that case? Or is it related to steep climbing turns where the engine turning in might suffer some airflow shadow affect?